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 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: 9 hours ago
TLE from 9 hours ago
0 GONETS M 09 (M19)
1 40062U 14036B 26061.91784014 .00000036 00000-0 18638-3 0 9993
2 40062 82.5139 13.6624 0024084 29.4244 330.8186 12.42947335529259Epoch: 2026-03-02T22:01Z
TLE epoch observation values (Epoch: 2026-03-02T22:01:41.388Z)
Latitude
0.00001°
Longitude
-117.46442°
Altitude
1,480.289 km
Speed
7.131 km/s
True Right ascension
00h 54m 38s
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
11:08:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,510.438 km
Perigee altitude
1,472.531 km
Semi-major axis
7,869.621 km
Eccentricity
0.00241
Inclination
82.5139°
RAAN
13.6624°
Arg. of periapsis
29.4244°
True anomaly
330.68368°
Mean anomaly
330.8186°
Eccentric anomaly
330.75118°
Mean motion
3.10894 °/min
Orbital period
115.8 mins
BSTAR
0.00018638
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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. |
|---|---|---|---|---|---|---|---|
| 16 mins | 2026-03-03 08:18:00.708Z | 356.955° N | 2026-03-03 08:26:00.708Z | 86.639° E | 43.581° | 2026-03-03 08:34:00.708Z | 164.426° S |
| 11 mins | 2026-03-03 10:17:00.708Z | 318.484° NNW | 2026-03-03 10:22:00.708Z | 277.448° WNW | 21.44° | 2026-03-03 10:28:00.708Z | 232.914° WSW |
| 7 mins | 2026-03-03 19:27:00.708Z | 99.11° ESE | 2026-03-03 19:30:00.708Z | 76.755° E | 14.612° | 2026-03-03 19:34:00.708Z | 47.76° ENE |
| 16 mins | 2026-03-03 21:18:00.708Z | 181.76° SSW | 2026-03-03 21:25:00.708Z | 147.209° SSE | 44.614° | 2026-03-03 21:34:00.708Z | 9.155° NNE |
| 10 mins | 2026-03-03 23:19:00.708Z | 261.176° W | 2026-03-03 23:23:00.708Z | 292.836° NW | 18.748° | 2026-03-03 23:29:00.708Z | 338.581° N |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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