DECAYED

OBJECT G, 47938 (Decayed)

Orbit data source: Space-Track

You're viewing an Uncataloged Satellite

Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.

OBJECT G, 47938 was a satellite in LEO that was launched on Mon, 22 Mar 2021 UTC via a SOYUZ-2-1A launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). Unknown objects in Earth's orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earth's gravity. This object's orbit decayed before it could be identified.

Not visible in the next 10 days
Identifier
47938, 2021-022G
Orbit
Decayed
Country
Flag of TBDTBD
Related business
None
Manufacturer
Unknown
Mission
Decayed Amateur Technology
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2021-03-22 (5 years ago)
Launch vehicle
SOYUZ-2-1A
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Unknown
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.025 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 1 year ago

TLE from 1 year ago
0 OBJECT G
1 47938U 21022G   25150.36328006  .08208755  25634-5  10107-2 0  9990
2 47938  97.3949  64.7229 0009697 222.3257 137.7293 16.36156971232361
Epoch: 2025-05-30T08:43Z
TLE epoch observation values (Epoch: 2025-05-30T08:43:07.397Z)
Latitude
-0.00001°
Longitude
45.82299°
Altitude
183.999 km
Speed
7.793 km/s
True Right ascension
04h 18m 53s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
21:33:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
179.21 km
Perigee altitude
166.505 km
Semi-major axis
6,550.995 km
Eccentricity
0.00097
Inclination
97.3949°
RAAN
64.7229°
Arg. of periapsis
222.3257°
True anomaly
137.80398°
Mean anomaly
137.7293°
Eccentric anomaly
137.76664°
Mean motion
4.09338 °/min
Orbital period
87.95 mins
BSTAR
0.0010107
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|