GONETS M 12 (M22), 40553
Orbit data source: Space-Track
GONETS M 12 (M22), 40553 is a payload satellite owned by Gonets (CIS) in LEO that was launched on Tue, 31 Mar 2015 UTC via an ROKOT launch vehicle from the Plesetsk Missile And Space Complex (PKMTR). 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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40553 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
Resehetnev ISS
Mission
Operational Commercial Communications
Bus & Motor
STRELA-3M, Unknown motor
Mass
225 kg wet, 225 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + 1 Ant, 3.5 m
Radar Cross Section
1.798 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 GONETS M 12 (M22)
1 40553U 15020B 25309.28067612 .00000049 00000-0 28073-3 0 9992
2 40553 82.4902 171.5630 0015312 113.1733 247.0962 12.42862446480919Epoch: 2025-11-05T06:44Z
TLE epoch observation values (Epoch: 2025-11-05T06:44:10.416Z)
Latitude
0.00002°
Longitude
25.764°
Altitude
1,501.9 km
Speed
7.111 km/s
True Right ascension
11h 26m 15s
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
11:09:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,503.894 km
Perigee altitude
1,479.793 km
Semi-major axis
7,869.981 km
Eccentricity
0.00153
Inclination
82.4902°
RAAN
171.563°
Arg. of periapsis
113.1733°
True anomaly
246.93469°
Mean anomaly
247.0962°
Eccentric anomaly
247.01543°
Mean motion
3.10873 °/min
Orbital period
115.8 mins
BSTAR
0.00028073
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Other satellites on launch #20 in the year 2015 (2015-03-31 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.GONETS M 12 (M22) 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. |
|---|---|---|---|---|---|---|---|
| 16 mins | 2025-11-05 16:28:56.858Z | 210.658° SW | 2025-11-05 16:36:56.858Z | 278.301° WNW | 37.165° | 2025-11-05 16:44:56.858Z | 356.291° N |
| 7 mins | 2025-11-06 00:46:56.858Z | 38.691° NE | 2025-11-06 00:49:56.858Z | 61.659° ENE | 15.333° | 2025-11-06 00:53:56.858Z | 91.134° ESE |
| 15 mins | 2025-11-06 02:40:56.858Z | 355.047° N | 2025-11-06 02:47:56.858Z | 62.267° ENE | 44.611° | 2025-11-06 02:55:56.858Z | 169.569° S |
| 9 mins | 2025-11-06 04:39:56.858Z | 312.342° NW | 2025-11-06 04:43:56.858Z | 280.336° WNW | 18.58° | 2025-11-06 04:48:56.858Z | 242.7° WSW |
| 9 mins | 2025-11-06 13:47:56.858Z | 109.921° ESE | 2025-11-06 13:51:56.858Z | 79.735° E | 17.229° | 2025-11-06 13:56:56.858Z | 42.516° NE |
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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