Showing default

GRUS-1D, 47936

Orbit data source: Space-Track

GRUS-1D, 47936 is a Japanese payload satellite in SSO that was launched on Mon, 22 Mar 2021 UTC via a SOYUZ-2-1A launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

Loading next visibility...
Identifier
47936, 2021-022E
Orbit
SSO
Country
Flag of JPJP / JPN
Related business
Manufacturer
AXELSPACE
Mission
Operational Commercial Imaging
Bus & Motor
GRUS, Unknown motor
Mass
80 kg wet, 80 kg dry
Launch date (UTC)
2021-03-22 (5 years ago)
Launch vehicle
SOYUZ-2-1A
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.3 m
Radar Cross Section
0.375 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 22 hours ago

TLE from 22 hours ago
0 GRUS-1D
1 47936U 21022E   26172.54024404  .00000791  00000-0  70492-4 0  9990
2 47936  97.5370  55.7905 0010497 293.7965  66.2157 14.98696539286558
Epoch: 2026-06-21T12:57Z
TLE epoch observation values (Epoch: 2026-06-21T12:57:57.085Z)
Latitude
-0.00002°
Longitude
-48.4364°
Altitude
571.044 km
Speed
7.577 km/s
True Right ascension
03h 43m 09s
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
21:46:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
575.214 km
Perigee altitude
560.631 km
Semi-major axis
6,946.06 km
Eccentricity
0.00105
Inclination
97.537°
RAAN
55.7905°
Arg. of periapsis
293.7965°
True anomaly
66.32583°
Mean anomaly
66.2157°
Eccentric anomaly
66.27076°
Mean motion
3.74917 °/min
Orbital period
96.02 mins
BSTAR
0.000070492
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|