GONETS D1 2, 23788
Orbit data source: Space-Track
GONETS D1 2, 23788 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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23788 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: 16 hours ago
TLE from 16 hours ago
0 GONETS D1 2
1 23788U 96009B 25361.23071988 .00000010 00000-0 -61671-5 0 9995
2 23788 82.5699 54.5309 0008126 99.9689 260.2320 12.63211326376381Epoch: 2025-12-27T05:32Z
TLE epoch observation values (Epoch: 2025-12-27T05:32:14.197Z)
Latitude
-0.00003°
Longitude
-124.48829°
Altitude
1,413.527 km
Speed
7.153 km/s
True Right ascension
03h 38m 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
21:23:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,413.364 km
Perigee altitude
1,400.711 km
Semi-major axis
7,785.174 km
Eccentricity
0.00081
Inclination
82.5699°
RAAN
54.5309°
Arg. of periapsis
99.9689°
True anomaly
260.14025°
Mean anomaly
260.232°
Eccentric anomaly
260.18612°
Mean motion
3.15966 °/min
Orbital period
113.94 mins
BSTAR
-0.0000061671
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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 2 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-12-28 02:35:33.418Z | 110.558° ESE | 2025-12-28 02:39:33.418Z | 80.609° E | 15.671° | 2025-12-28 02:43:33.418Z | 49.231° ENE |
| 15 mins | 2025-12-28 04:26:33.418Z | 185.316° SSW | 2025-12-28 04:33:33.418Z | 192.896° SSW | 44.998° | 2025-12-28 04:41:33.418Z | 7.716° NNE |
| 9 mins | 2025-12-28 06:25:33.418Z | 263.839° W | 2025-12-28 06:29:33.418Z | 295.521° NW | 16.869° | 2025-12-28 06:34:33.418Z | 334.254° NNW |
| 13 mins | 2025-12-28 14:28:33.418Z | 14.349° NNE | 2025-12-28 14:34:33.418Z | 74.099° E | 30.763° | 2025-12-28 14:41:33.418Z | 135.987° SSE |
| 13 mins | 2025-12-28 16:23:33.418Z | 334.81° NNW | 2025-12-28 16:29:33.418Z | 269.808° W | 35.579° | 2025-12-28 16:36:33.418Z | 204.225° SW |
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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