GONETS M 10 (M20), 40063
Orbit data source: Space-Track
GONETS M 10 (M20), 40063 is a payload satellite owned by Gonets (CIS) in LEO that was launched on Thu, 03 Jul 2014 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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40063 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
Resehetnev ISS
Mission
Operational Commercial Communications
Bus & Motor
STRELA-3M, Unknown motor
Mass
280 kg wet, 280 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: 1 day ago
TLE from 1 day ago
0 GONETS M 10 (M20)
1 40063U 14036C 26297.26194802 -.00000023 00000-0 -23522-3 0 9999
2 40063 82.5113 227.4898 0020640 219.1538 140.8050 12.42948507558284Epoch: 2026-10-24T06:17Z
TLE epoch observation values (Epoch: 2026-10-24T06:17:12.308Z)
Latitude
0.00003°
Longitude
100.51785°
Altitude
1,509.437 km
Speed
7.104 km/s
True Right ascension
15h 09m 57s
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
10:50:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,507.722 km
Perigee altitude
1,475.237 km
Semi-major axis
7,869.617 km
Eccentricity
0.00206
Inclination
82.5113°
RAAN
227.4898°
Arg. of periapsis
219.1538°
True anomaly
140.95417°
Mean anomaly
140.805°
Eccentric anomaly
140.87962°
Mean motion
3.10894 °/min
Orbital period
115.79 mins
BSTAR
-0.00023522
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Other satellites on launch #36 in the year 2014 (2014-07-03 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 10 (M20) 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. |
|---|---|---|---|---|---|---|---|
| 15 mins | 2026-10-25 19:04:51.446Z | 149.438° SSE | 2026-10-25 19:12:51.446Z | 79.365° E | 39.113° | 2026-10-25 19:19:51.446Z | 23.457° NE |
| 15 mins | 2026-10-25 21:01:51.446Z | 218.015° SW | 2026-10-25 21:08:51.446Z | 282.403° WNW | 44.964° | 2026-10-25 21:16:51.446Z | 354.954° N |
| 9 mins | 2026-10-26 05:17:51.446Z | 31.179° NE | 2026-10-26 05:21:51.446Z | 61.88° ENE | 18.094° | 2026-10-26 05:26:51.446Z | 99.208° ESE |
| 15 mins | 2026-10-26 07:12:51.446Z | 352.883° N | 2026-10-26 07:19:51.446Z | 21.086° NNE | 86.864° | 2026-10-26 07:27:51.446Z | 173.96° S |
| 8 mins | 2026-10-26 09:11:51.446Z | 310.758° NW | 2026-10-26 09:15:51.446Z | 280.09° WNW | 17.434° | 2026-10-26 09:19:51.446Z | 250.482° W |
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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