GONETS M 09 (M19), 40062
Orbit data source: Space-Track
GONETS M 09 (M19), 40062 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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40062 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: 7 hours ago
TLE from 7 hours ago
0 GONETS M 09 (M19)
1 40062U 14036B 26283.91727547 -.00000021 00000-0 -21941-3 0 9994
2 40062 82.5086 235.7573 0021762 264.1597 95.7001 12.42953966556833Epoch: 2026-10-10T22:00Z
TLE epoch observation values (Epoch: 2026-10-10T22:00:52.600Z)
Latitude
-0.00012°
Longitude
-113.97941°
Altitude
1,498.544 km
Speed
7.114 km/s
True Right ascension
15h 43m 01s
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
23:21:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,508.582 km
Perigee altitude
1,474.331 km
Semi-major axis
7,869.594 km
Eccentricity
0.00218
Inclination
82.5086°
RAAN
235.7573°
Arg. of periapsis
264.1597°
True anomaly
95.94817°
Mean anomaly
95.7001°
Eccentric anomaly
95.82414°
Mean motion
3.10896 °/min
Orbital period
115.79 mins
BSTAR
-0.00021941
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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 09 (M19) 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-10-11 06:24:16.145Z | 42.205° NE | 2026-10-11 06:26:16.145Z | 55.699° ENE | 10.849° | 2026-10-11 06:28:16.145Z | 69.217° E |
| 15 mins | 2026-10-11 08:18:16.145Z | 2.423° NNE | 2026-10-11 08:25:16.145Z | 79.878° E | 60.377° | 2026-10-11 08:33:16.145Z | 156.631° SSE |
| 13 mins | 2026-10-11 10:15:16.145Z | 327.433° NNW | 2026-10-11 10:21:16.145Z | 278.715° WNW | 28.583° | 2026-10-11 10:28:16.145Z | 223.738° SW |
| 4 mins | 2026-10-11 19:28:16.145Z | 82.82° E | 2026-10-11 19:29:16.145Z | 75.847° E | 11.866° | 2026-10-11 19:32:16.145Z | 55.323° ENE |
| 16 mins | 2026-10-11 21:17:16.145Z | 173.219° S | 2026-10-11 21:24:16.145Z | 110.185° ESE | 70.155° | 2026-10-11 21:33:16.145Z | 12.145° NNE |
| 11 mins | 2026-10-11 23:17:16.145Z | 251.405° W | 2026-10-11 23:22:16.145Z | 293.614° NW | 24.948° | 2026-10-11 23:28:16.145Z | 341.183° N |
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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