GRUS-1A, 43890
Orbit data source: Space-Track
GRUS-1A, 43890 is a payload satellite in SSO that was launched on Thu, 27 Dec 2018 UTC via a SOYUZ-2-1A launch vehicle from the Vostochny Cosmodrome (VOSTO). 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.
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43890 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
Manufacturer
AXELSPACE
Mission
Operational Commercial Imaging
Bus & Motor
GRUS, Unknown motor
Mass
80 kg wet, 80 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.3 m
Radar Cross Section
0.375 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 GRUS-1A
1 43890U 18111Q 26050.61211681 .00000624 00000-0 56296-4 0 9999
2 43890 97.4719 282.7619 0007775 181.8201 178.2995 14.98838251390096Epoch: 2026-02-19T14:41Z
TLE epoch observation values (Epoch: 2026-02-19T14:41:26.892Z)
Latitude
-0.00006°
Longitude
-87.16105°
Altitude
578.946 km
Speed
7.568 km/s
True Right ascension
18h 51m 02s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
23:01:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.882 km
Perigee altitude
562.081 km
Semi-major axis
6,945.619 km
Eccentricity
0.00078
Inclination
97.4719°
RAAN
282.7619°
Arg. of periapsis
181.8201°
True anomaly
178.30214°
Mean anomaly
178.2995°
Eccentric anomaly
178.30082°
Mean motion
3.74953 °/min
Orbital period
96.01 mins
BSTAR
0.000056296
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Other satellites on launch #111 in the year 2018 (2018-12-27 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.GRUS-1A Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-02-20 04:04:47.447Z | 19.808° NNE | 2026-02-20 04:07:47.447Z | 87.514° E | 42.488° | 2026-02-20 04:11:47.447Z | 183.998° SSW |
| 5 mins | 2026-02-20 14:52:47.447Z | 120.687° SE | 2026-02-20 14:54:47.447Z | 67.843° E | 29.909° | 2026-02-20 14:57:47.447Z | 9.992° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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