GONETS D1 1, 23787
Orbit data source: Space-Track
GONETS D1 1, 23787 is a payload satellite owned by Gonets (CIS) in LEO that was launched on Mon, 19 Feb 1996 UTC via a TSIKLON-3 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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23787 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
NPO PM
Mission
Non-operational Civil Communications
Bus & Motor
STRELA-3, Unknown motor
Mass
225 kg wet, 225 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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 GONETS D1 1
1 23787U 96009A 25355.20966818 .00000037 00000-0 14468-3 0 9997
2 23787 82.5770 52.8710 0012275 88.6866 326.7606 12.64102055376822Epoch: 2025-12-21T05:01Z
TLE epoch observation values (Epoch: 2025-12-21T05:01:55.330Z)
Latitude
54.7727°
Longitude
-102.05585°
Altitude
1,407.06 km
Speed
7.165 km/s
True Right ascension
04h 13m 48s
True Declination
54° 37' 27"
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
11:12:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,412.929 km
Perigee altitude
1,393.825 km
Semi-major axis
7,781.514 km
Eccentricity
0.00123
Inclination
82.577°
RAAN
52.871°
Arg. of periapsis
88.6866°
True anomaly
326.6834°
Mean anomaly
326.7606°
Eccentric anomaly
326.72201°
Mean motion
3.16189 °/min
Orbital period
113.86 mins
BSTAR
0.00014468
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Other satellites on launch #9 in the year 1996 (1996-02-19 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 D1 1 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 | 2025-12-21 14:50:41.803Z | 9.979° NNE | 2025-12-21 14:57:41.803Z | 74.356° E | 30.625° | 2025-12-21 15:04:41.803Z | 135.958° SSE |
| 13 mins | 2025-12-21 16:46:41.803Z | 334.562° NNW | 2025-12-21 16:52:41.803Z | 267.87° W | 35.62° | 2025-12-21 16:59:41.803Z | 203.742° SW |
| 13 mins | 2025-12-22 03:38:41.803Z | 142.718° SSE | 2025-12-22 03:44:41.803Z | 86.575° E | 30.159° | 2025-12-22 03:51:41.803Z | 25.266° NE |
| 14 mins | 2025-12-22 05:32:41.803Z | 216.272° SW | 2025-12-22 05:39:41.803Z | 291.439° WNW | 35.785° | 2025-12-22 05:46:41.803Z | 355.086° 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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