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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
FENGYUN 3E
1st orbit: 2021 Jul 4
202149008U99827825101Tracking
2021-062B
1st orbit: 2021 Jul 5
202149009U99859728101Tracking
CZ-4C R/B
1st orbit: 2021 Jul 4
202149010U9980561399Tracking
TIANLIAN 1-05
1st orbit: 2021 Jul 10
202149011U335790357811436Tracking
CZ-3C R/B
1st orbit: 2021 Jul 2
202149012U1839627181707Tracking
ORCA-7
1st orbit: 2021 Jun 30
202149013U5250248895Tracking
GUNSMOKE-J 2
1st orbit: 2021 Jun 30
202149014U5250248895Tracking
ORCA-6
1st orbit: 2021 Jun 30
202149015U5250348795Tracking
DHABISAT (MYSAT-2)
1st orbit: 2021 Jun 29
202149016U5250249295Tracking
IT-SPINS
1st orbit: 2021 Jun 29
202149017U5250249295Tracking
NINGXIA-1 6
1st orbit: 2021 Jul 9
202149018U45872860102Tracking
NINGXIA-1 7
1st orbit: 2021 Jul 9
202149019U45870860102Tracking
NINGXIA-1 8
1st orbit: 2021 Jul 9
202149020U45870858102Tracking
NINGXIA-1 9
1st orbit: 2021 Jul 9
202149021U45869857102Tracking
NINGXIA-1 10
1st orbit: 2021 Jul 9
202149022U45868856102Tracking
CZ-6 R/B
1st orbit: 2021 Jul 9
202149023U45887638100Tracking
2021-062D
1st orbit: 2021 Jul 9
202149024U99804799101Tracking
YAOGAN-30 AD
1st orbit: 2021 Jul 19
202149026U3560559897Tracking
TIANQI-15
1st orbit: 2021 Jul 18
202149027U3559958897Tracking
YAOGAN-30 AE
1st orbit: 2021 Jul 19
202149028U3561160697Tracking
YAOGAN-30 AF
1st orbit: 2021 Jul 18
202149029U3560058997Tracking
CZ-2C R/B
1st orbit: 2021 Jul 19
202149030U3559346295Tracking
ISS (NAUKA)
1st orbit: 2016 May 10
202149044U5242141993Tracking
SL-25 R/B
1st orbit: 2021 Jul 21
202149045U5223716989Tracking
2021-062E
1st orbit: 2021 Jul 20
202149047U99804799101Tracking
2021-067A
1st orbit: 2021 Jul 29
202149049U9750348895Tracking
2021-068A
1st orbit: 2021 Jul 29
202149052U3761059897Tracking
2021-068B
1st orbit: 2021 Jul 29
202149053U3760524193Tracking
2021-068C
1st orbit: 2021 Jul 29
202149054U3759434494Tracking
2021-069A
1st orbit: 2021 Jul 31
202149055U335708250631Tracking
2021-069B
1st orbit: 2021 Jul 31
202149056U335549228627Tracking
2021-069C
1st orbit: 2021 Jul 31
202149057U335723238631Tracking
2021-069D
1st orbit: 2021 Jul 31
202149058U335557229627Tracking
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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