GONETS M 08 (M18), 40061
Orbit data source: Space-Track
GONETS M 08 (M18), 40061 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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40061 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
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: 5 hours ago
TLE from 5 hours ago
0 GONETS M 08 (M18)
1 40061U 14036A 25343.65175591 .00000110 00000-0 71913-3 0 9997
2 40061 82.5115 65.3235 0029922 200.4523 159.5361 12.42978037518905Epoch: 2025-12-09T15:38Z
TLE epoch observation values (Epoch: 2025-12-09T15:38:31.710Z)
Latitude
-0.00001°
Longitude
112.058°
Altitude
1,518.785 km
Speed
7.096 km/s
True Right ascension
04h 21m 17s
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
18:41:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,514.902 km
Perigee altitude
1,467.808 km
Semi-major axis
7,869.492 km
Eccentricity
0.00299
Inclination
82.5115°
RAAN
65.3235°
Arg. of periapsis
200.4523°
True anomaly
159.65556°
Mean anomaly
159.5361°
Eccentric anomaly
159.59587°
Mean motion
3.10902 °/min
Orbital period
115.79 mins
BSTAR
0.00071913
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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 08 (M18) 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 | 2025-12-10 05:15:14.171Z | 147.953° SSE | 2025-12-10 05:23:14.171Z | 80.111° E | 31.282° | 2025-12-10 05:30:14.171Z | 24.298° NE |
| 15 mins | 2025-12-10 07:12:14.171Z | 216.181° SW | 2025-12-10 07:19:14.171Z | 281.728° WNW | 36.21° | 2025-12-10 07:27:14.171Z | 355.621° N |
| 9 mins | 2025-12-10 15:28:14.171Z | 31.833° NE | 2025-12-10 15:32:14.171Z | 62.231° ENE | 16.316° | 2025-12-10 15:37:14.171Z | 98.679° ESE |
| 15 mins | 2025-12-10 17:23:14.171Z | 353.883° N | 2025-12-10 17:30:14.171Z | 60.544° ENE | 44.884° | 2025-12-10 17:38:14.171Z | 172.046° S |
| 8 mins | 2025-12-10 19:22:14.171Z | 311.019° NW | 2025-12-10 19:26:14.171Z | 279.583° WNW | 17.41° | 2025-12-10 19:30:14.171Z | 249.229° 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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