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 25355.13210021 .00000037 00000-0 14419-3 0 9994
2 23788 82.5704 58.4338 0008107 112.1326 248.0627 12.63211120375619Epoch: 2025-12-21T03:10Z
TLE epoch observation values (Epoch: 2025-12-21T03:10:13.458Z)
Latitude
0.00001°
Longitude
-79.07122°
Altitude
1,414.813 km
Speed
7.152 km/s
True Right ascension
03h 53m 44s
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
11:15:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,413.35 km
Perigee altitude
1,400.727 km
Semi-major axis
7,785.175 km
Eccentricity
0.00081
Inclination
82.5704°
RAAN
58.4338°
Arg. of periapsis
112.1326°
True anomaly
247.97656°
Mean anomaly
248.0627°
Eccentric anomaly
248.01963°
Mean motion
3.15966 °/min
Orbital period
113.94 mins
BSTAR
0.00014419
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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. |
|---|---|---|---|---|---|---|---|
| 14 mins | 2025-12-21 15:11:14.467Z | 11.462° NNE | 2025-12-21 15:18:14.467Z | 77.974° E | 30.077° | 2025-12-21 15:25:14.467Z | 136.116° SSE |
| 14 mins | 2025-12-21 17:06:14.467Z | 337.91° N | 2025-12-21 17:13:14.467Z | 264.298° W | 36.056° | 2025-12-21 17:20:14.467Z | 202.442° SSW |
| 12 mins | 2025-12-22 04:00:14.467Z | 138.507° SSE | 2025-12-22 04:05:14.467Z | 90.247° ESE | 29.8° | 2025-12-22 04:12:14.467Z | 26.574° NE |
| 13 mins | 2025-12-22 05:54:14.467Z | 218.166° SW | 2025-12-22 06:00:14.467Z | 284.702° WNW | 36.285° | 2025-12-22 06:07:14.467Z | 354.224° 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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