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Recently Launched Satellites
In this category are all objects launched in the last 30 days and includes cargo resupply to the ISS (International Space Station) as well as those satellites placed in orbit from the ISS. Most of the satellites seen in this list are geostationary communications equipment.
Satellite Launch Norad Incl.
degrees
Apogee
Km
Perigee
Km
Period
min
Options
WEINA 1A
1st orbit: 2018 Jan 25
201843169U3560159697Tracking
YAOGAN-30 K
1st orbit: 2018 Jan 25
201843170U3560459597Tracking
YAOGAN-30 L
1st orbit: 2018 Jan 25
201843171U3560159897Tracking
YAOGAN-30 M
1st orbit: 2018 Jan 25
201843172U3560259797Tracking
CZ-2C R/B
1st orbit: 2018 Jan 25
201843173U3560439495Tracking
AL YAH 3
1st orbit: 2018 Jan 13
201843174U647430233441416Tracking
SES-14
1st orbit: 2018 Jan 22
201843175U17481302856944Tracking
ARIANE 5 R/B
1st orbit: 2018 Jan 25
201843176U2142738200771Tracking
ARIANE 5 DEB [SYLDA]
1st orbit: 2018 Jan 25
201843177U2142988226777Tracking
KANOPUS-V 3
1st orbit: 2018 Feb 1
201843180U9751050695Tracking
KANOPUS-V 4
1st orbit: 2018 Feb 1
201843181U9751050195Tracking
LEMUR-2-JIN-LUEN
1st orbit: 2018 Feb 1
201843182U9859057196Tracking
LEMUR-2-URAMCHANSOL
1st orbit: 2018 Feb 1
201843183U9858957196Tracking
LEMUR-2-ADI
1st orbit: 2018 Feb 1
201843184U9858957196Tracking
LEMUR-2-THENICKMOLO
1st orbit: 2018 Feb 1
201843185U9858957196Tracking
2018-014G
1st orbit: 2018 Feb 1
201843186U9858557196Tracking
2018-014H
1st orbit: 2018 Feb 1
201843187U9858657096Tracking
D-STAR ONE PHOENIX
1st orbit: 2018 Feb 1
201843188U9858557196Tracking
2018-014K
1st orbit: 2018 Feb 11
201843189U9858557196Tracking
FENGMANIU-1 (FMN-1)
1st orbit: 2018 Feb 2
201843192U9751048795Tracking
2018-015B
1st orbit: 2018 Feb 2
201843193U9750349395Tracking
ZHANGZHENG-1 (CSES)
1st orbit: 2018 Feb 2
201843194U9750948695Tracking
NUSAT-4 (ADA)
1st orbit: 2018 Feb 2
201843195U9750948595Tracking
GOMX4-B
1st orbit: 2018 Feb 2
201843196U9750848295Tracking
GOMX4-A
1st orbit: 2018 Feb 2
201843197U9750848395Tracking
2018-015G
1st orbit: 2018 Feb 2
201843198U9750844094Tracking
SHAONIAN XING
1st orbit: 2018 Feb 2
201843199U9750848495Tracking
2018-015J
1st orbit: 2018 Feb 2
201843200U9749845594Tracking
TRICOM-1R (TASUKI)
1st orbit: 2018 Feb 3
201843201U311889186106Tracking
SS-520-5 R/B
1st orbit: 2018 Feb 3
201843202U311865184106Tracking
NUSAT-5 (MARYAM)
1st orbit: 2018 Feb 4
201843204U9750948595Tracking
TESLA ROADSTER
1st orbit: 2018 Feb 6
201843205U296939180164Tracking
BEIDOU-3 M5
1st orbit: 2018 Feb 12
201843207U552219121533787Tracking
BEIDOU-3 M6
1st orbit: 2018 Feb 12
201843208U552219121544787Tracking
CZ-3B R/B
1st orbit: 2018 Feb 12
201843209U5518481163326Tracking
YZ-1 R/B
1st orbit: 2018 Feb 12
201843210U552235322184804Tracking
PROGRESS-MS 08
1st orbit: 2016 May 15
201843211U5240740293Tracking
Satellites Orbital Parameters

The table above shows the main parameters and information available for this satellite.

Satellite: This column shows the name of the object in orbit. In some cases the official name ends with the words R/B, meaning that it is a piece or any stage from some rocket booster.

Norad: North American Aerospace Defense Command, the Air Defence Command of the United States, responsible for the catalogue of objects in orbit. The number indicates the record of the satellite in the Norad archives.

Inclination: Angle formed between the orbit of the satellite and terrestrial line of the equator. Satellites with inclination of 0 degrees follow the equator line and are called equatorial orbit satellites. When the inclination is 90 degrees its orbit crosses the terrestrial poles and are called polar orbiting satellites. When the inclination is less or equal latitude of the place of observation, the satellite be seen directly if conditions permit.

Apogee: Maximum distance that the object is far from the center of the Earth.

Perigee: Highest approchement between the object and the center of the Earth. The figures shown already discounting the radius of the Earth, 6378 Km. One Perigee value equal to the value of Apogee indicates a circular orbit satellite.

Period: Value in minutes that a satellite takes to complete one orbit of perigee to perigee. Satellites in polar orbit, positioned at 800 km in altitude will take approximately 102 minutes to complete one revolution. The International Space Station, 350 km above the surface, completes its orbit in 90 minutes.

The lower the altitude of a satellite, more speed he needs to keep in orbit and not re-enters the atmosphere.

Geostationary satellites have a period of approximately 1436 minutes with inclination of 0 degrees (equatorial orbit). Because this is the same time it takes Earth to complete one turn on its axis, geostationary satellites appear static on the same geographic point. To this happens the satellite should be positioned about 36 thousand kilometers in altitude.

Note and Frequency: Filled with additional information where possible. The frequencies shown, when provided, are those captured by enthusiasts or informed by the official organizations of disclosure.

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