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: 15 hours ago
TLE from 15 hours ago
0 GONETS D1 2
1 23788U 96009B 25260.00930240 .00000029 00000-0 10158-3 0 9994
2 23788 82.5675 119.3126 0006780 336.6127 23.4655 12.63206834363603Epoch: 2025-09-17T00:13Z
TLE epoch observation values (Epoch: 2025-09-17T00:13:23.727Z)
Latitude
-0.00004°
Longitude
119.77233°
Altitude
1,407.623 km
Speed
7.159 km/s
True Right ascension
07h 57m 15s
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
07:33:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,412.334 km
Perigee altitude
1,401.778 km
Semi-major axis
7,785.193 km
Eccentricity
0.00068
Inclination
82.5675°
RAAN
119.3126°
Arg. of periapsis
336.6127°
True anomaly
23.49646°
Mean anomaly
23.4655°
Eccentric anomaly
23.48098°
Mean motion
3.15965 °/min
Orbital period
113.94 mins
BSTAR
0.00010158
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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 | 2025-09-17 15:30:30.858Z | 187.851° SSW | 2025-09-17 15:38:30.858Z | 264.811° W | 44.886° | 2025-09-17 15:46:30.858Z | 6.55° NNE |
| 8 mins | 2025-09-17 17:31:30.858Z | 271.632° WNW | 2025-09-17 17:34:30.858Z | 295.38° NW | 15.74° | 2025-09-17 17:39:30.858Z | 333.371° NNW |
| 13 mins | 2025-09-18 01:33:30.858Z | 12.738° NNE | 2025-09-18 01:39:30.858Z | 72.875° E | 32.338° | 2025-09-18 01:46:30.858Z | 137.958° SSE |
| 13 mins | 2025-09-18 03:28:30.858Z | 333.589° NNW | 2025-09-18 03:34:30.858Z | 271.467° WNW | 34.177° | 2025-09-18 03:41:30.858Z | 207.026° SW |
| 13 mins | 2025-09-18 14:21:30.858Z | 143.427° SSE | 2025-09-18 14:27:30.858Z | 79.831° E | 31.866° | 2025-09-18 14:34:30.858Z | 22.646° NE |
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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