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: 9 hours ago
TLE from 9 hours ago
0 GONETS D1 2
1 23788U 96009B 25300.48205634 .00000038 00000-0 15187-3 0 9990
2 23788 82.5662 93.4031 0006363 231.9170 128.1348 12.63208685368713Epoch: 2025-10-27T11:34Z
TLE epoch observation values (Epoch: 2025-10-27T11:34:09.667Z)
Latitude
-0.00005°
Longitude
-116.22046°
Altitude
1,415.522 km
Speed
7.151 km/s
True Right ascension
06h 13m 36s
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
16:19:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,412.002 km
Perigee altitude
1,402.095 km
Semi-major axis
7,785.185 km
Eccentricity
0.00064
Inclination
82.5662°
RAAN
93.4031°
Arg. of periapsis
231.917°
True anomaly
128.19212°
Mean anomaly
128.1348°
Eccentric anomaly
128.16346°
Mean motion
3.15966 °/min
Orbital period
113.94 mins
BSTAR
0.00015187
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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. |
|---|---|---|---|---|---|---|---|
| 16 mins | 2025-10-27 21:40:14.071Z | 359.799° N | 2025-10-27 21:48:14.071Z | 74.688° E | 40.254° | 2025-10-27 21:56:14.071Z | 155.841° SSE |
| 12 mins | 2025-10-27 23:37:14.071Z | 325.295° NNW | 2025-10-27 23:42:14.071Z | 282.361° WNW | 25.263° | 2025-10-27 23:49:14.071Z | 223.176° SW |
| 14 mins | 2025-10-28 10:29:14.071Z | 162.754° S | 2025-10-28 10:35:14.071Z | 96.129° ESE | 40.246° | 2025-10-28 10:43:14.071Z | 15.894° NNE |
| 12 mins | 2025-10-28 12:25:14.071Z | 239.893° WSW | 2025-10-28 12:31:14.071Z | 295.865° NW | 25.903° | 2025-10-28 12:37:14.071Z | 345.621° N |
| 10 mins | 2025-10-28 20:31:14.071Z | 27.502° NE | 2025-10-28 20:35:14.071Z | 61.599° ENE | 21.055° | 2025-10-28 20:41:14.071Z | 111.74° ESE |
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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