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: 12 hours ago
TLE from 12 hours ago
0 GONETS D1 2
1 23788U 96009B 25260.72213000 .00000035 00000-0 13561-3 0 9999
2 23788 82.5673 118.8564 0006754 334.9209 25.1553 12.63206890363691Epoch: 2025-09-17T17:19Z
TLE epoch observation values (Epoch: 2025-09-17T17:19:52.032Z)
Latitude
-0.00006°
Longitude
-138.00441°
Altitude
1,407.705 km
Speed
7.159 km/s
True Right ascension
07h 55m 25s
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
22:16:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,412.314 km
Perigee altitude
1,401.798 km
Semi-major axis
7,785.193 km
Eccentricity
0.00068
Inclination
82.5673°
RAAN
118.8564°
Arg. of periapsis
334.9209°
True anomaly
25.18822°
Mean anomaly
25.1553°
Eccentric anomaly
25.17176°
Mean motion
3.15965 °/min
Orbital period
113.94 mins
BSTAR
0.00013561
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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 | 2025-09-18 14:19:56.470Z | 149.78° SSE | 2025-09-18 14:26:56.470Z | 88.75° E | 31.981° | 2025-09-18 14:33:56.470Z | 24.525° NE |
| 13 mins | 2025-09-18 16:15:56.470Z | 222.481° SW | 2025-09-18 16:21:56.470Z | 286.902° WNW | 34.3° | 2025-09-18 16:28:56.470Z | 352.991° N |
| 6 mins | 2025-09-19 00:23:56.470Z | 40.945° NE | 2025-09-19 00:26:56.470Z | 64.349° ENE | 14.238° | 2025-09-19 00:29:56.470Z | 86.927° E |
| 15 mins | 2025-09-19 02:15:56.470Z | 356.048° N | 2025-09-19 02:22:56.470Z | 85.8° E | 44.386° | 2025-09-19 02:30:56.470Z | 168.393° S |
| 9 mins | 2025-09-19 04:12:56.470Z | 312.706° NW | 2025-09-19 04:16:56.470Z | 279.218° WNW | 18.915° | 2025-09-19 04:21:56.470Z | 240.309° WSW |
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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