GONETS M 07, 39251
Orbit data source: Space-Track
GONETS M 07, 39251 is a payload satellite owned by Gonets (CIS) in LEO that was launched on Wed, 11 Sep 2013 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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39251 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: 14 hours ago
TLE from 14 hours ago
0 GONETS M 07
1 39251U 13048C 25272.27210759 .00000015 00000-0 38538-4 0 9994
2 39251 82.4896 148.8352 0018138 62.5187 297.7734 12.42902853546426Epoch: 2025-09-29T06:31Z
TLE epoch observation values (Epoch: 2025-09-29T06:31:50.095Z)
Latitude
-0.00004°
Longitude
42.59826°
Altitude
1,490.387 km
Speed
7.122 km/s
True Right ascension
09h 55m 20s
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
14:22:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,505.948 km
Perigee altitude
1,477.399 km
Semi-major axis
7,869.81 km
Eccentricity
0.00181
Inclination
82.4896°
RAAN
148.8352°
Arg. of periapsis
62.5187°
True anomaly
297.5893°
Mean anomaly
297.7734°
Eccentric anomaly
297.68137°
Mean motion
3.10883 °/min
Orbital period
115.8 mins
BSTAR
0.000038538
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Other satellites on launch #48 in the year 2013 (2013-09-11 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 07 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. |
|---|---|---|---|---|---|---|---|
| 14 mins | 2025-09-30 02:27:31.868Z | 10.792° NNE | 2025-09-30 02:34:31.868Z | 68.303° E | 28.456° | 2025-09-30 02:41:31.868Z | 128.699° SE |
| 15 mins | 2025-09-30 04:24:31.868Z | 341.084° N | 2025-09-30 04:31:31.868Z | 277.159° WNW | 38.7° | 2025-09-30 04:39:31.868Z | 198.064° SSW |
| 14 mins | 2025-09-30 15:28:31.868Z | 146.014° SSE | 2025-09-30 15:35:31.868Z | 81.383° E | 31.595° | 2025-09-30 15:42:31.868Z | 24.018° NE |
| 14 mins | 2025-09-30 17:25:31.868Z | 220.369° SW | 2025-09-30 17:31:31.868Z | 279.954° WNW | 35.322° | 2025-09-30 17:39:31.868Z | 355.099° 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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