GONETS M 11 (M21), 40552
Orbit data source: Space-Track
GONETS M 11 (M21), 40552 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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40552 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
Resehetnev ISS
Mission
Operational Civil 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: 7 hours ago
TLE from 7 hours ago
0 GONETS M 11 (M21)
1 40552U 15020A 25243.61749875 .00000050 00000-0 28982-3 0 9994
2 40552 82.4854 211.3819 0014679 276.7480 83.1929 12.42862550472768Epoch: 2025-08-31T14:49Z
TLE epoch observation values (Epoch: 2025-08-31T14:49:11.891Z)
Latitude
-0.00006°
Longitude
9.04748°
Altitude
1,495.838 km
Speed
7.117 km/s
True Right ascension
14h 05m 31s
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
13:52:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,503.396 km
Perigee altitude
1,480.291 km
Semi-major axis
7,869.981 km
Eccentricity
0.00147
Inclination
82.4854°
RAAN
211.3819°
Arg. of periapsis
276.748°
True anomaly
83.35996°
Mean anomaly
83.1929°
Eccentric anomaly
83.27643°
Mean motion
3.10873 °/min
Orbital period
115.8 mins
BSTAR
0.00028982
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Other satellites on launch #20 in the year 2015 (2015-03-31 UTC)
GONETS M 11 (M21) Visibility forecast
Observer location: undefined°, undefined°
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. |
|---|---|---|---|---|---|---|---|
| 17 mins | 2025-08-31 22:37:04.565Z | 183.418° SSW | 2025-08-31 22:46:04.565Z | 42.476° NE | 44.876° | 2025-08-31 22:54:04.565Z | 8.602° NNE |
| 10 mins | 2025-09-01 00:39:04.565Z | 260.113° W | 2025-09-01 00:44:04.565Z | 298.91° NW | 18.453° | 2025-09-01 00:49:04.565Z | 336.229° NNW |
| 14 mins | 2025-09-01 08:50:04.565Z | 9.75° NNE | 2025-09-01 08:57:04.565Z | 78.75° E | 33.868° | 2025-09-01 09:04:04.565Z | 140.094° SSE |
| 14 mins | 2025-09-01 10:47:04.565Z | 333.902° NNW | 2025-09-01 10:53:04.565Z | 279.927° WNW | 33.473° | 2025-09-01 11:01:04.565Z | 208.117° SW |
| 14 mins | 2025-09-01 21:50:04.565Z | 155.805° SSE | 2025-09-01 21:57:04.565Z | 81.781° E | 37.132° | 2025-09-01 22:04:04.565Z | 20.249° 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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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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Authenticating...
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