GONETS M 05, 39249
Orbit data source: Space-Track
GONETS M 05, 39249 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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39249 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: 12 hours ago
TLE from 12 hours ago
0 GONETS M 05
1 39249U 13048A 25272.30384007 .00000030 00000-0 14592-3 0 9993
2 39249 82.4826 146.0303 0017281 61.4771 298.8046 12.42869886546478Epoch: 2025-09-29T07:17Z
TLE epoch observation values (Epoch: 2025-09-29T07:17:31.782Z)
Latitude
-0°
Longitude
28.33839°
Altitude
1,490.622 km
Speed
7.122 km/s
True Right ascension
09h 44m 07s
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
12:24:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,505.413 km
Perigee altitude
1,478.213 km
Semi-major axis
7,869.95 km
Eccentricity
0.00173
Inclination
82.4826°
RAAN
146.0303°
Arg. of periapsis
61.4771°
True anomaly
298.6309°
Mean anomaly
298.8046°
Eccentric anomaly
298.71777°
Mean motion
3.10875 °/min
Orbital period
115.8 mins
BSTAR
0.00014592
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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 05 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-09-30 01:19:05.764Z | 32.699° NE | 2025-09-30 01:23:05.764Z | 60.973° ENE | 13.078° | 2025-09-30 01:26:05.764Z | 82.2° E |
| 15 mins | 2025-09-30 03:14:05.764Z | 358.002° N | 2025-09-30 03:21:05.764Z | 68.054° E | 43.375° | 2025-09-30 03:29:05.764Z | 163.435° S |
| 11 mins | 2025-09-30 05:12:05.764Z | 320.962° NNW | 2025-09-30 05:17:05.764Z | 281.184° WNW | 21.586° | 2025-09-30 05:23:05.764Z | 234.439° WSW |
| 6 mins | 2025-09-30 14:23:05.764Z | 95.077° ESE | 2025-09-30 14:26:05.764Z | 72.44° E | 14.361° | 2025-09-30 14:29:05.764Z | 50.758° ENE |
| 15 mins | 2025-09-30 16:14:05.764Z | 180.964° SSW | 2025-09-30 16:21:05.764Z | 82.074° E | 44.786° | 2025-09-30 16:29:05.764Z | 9.486° NNE |
| 10 mins | 2025-09-30 18:14:05.764Z | 258.025° W | 2025-09-30 18:19:05.764Z | 297.65° NW | 19.1° | 2025-09-30 18:24:05.764Z | 336.105° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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