GONETS D1 3, 23789
Orbit data source: Space-Track
GONETS D1 3, 23789 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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23789 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 3
1 23789U 96009C 25310.79730550 .00000025 00000-0 81993-4 0 9991
2 23789 82.5752 101.8534 0005141 200.2557 159.8331 12.62678464369581Epoch: 2025-11-06T19:08Z
TLE epoch observation values (Epoch: 2025-11-06T19:08:07.195Z)
Latitude
-0.00001°
Longitude
128.57295°
Altitude
1,418.399 km
Speed
7.15 km/s
True Right ascension
06h 47m 24s
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
00:11:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,413.232 km
Perigee altitude
1,405.225 km
Semi-major axis
7,787.366 km
Eccentricity
0.00051
Inclination
82.5752°
RAAN
101.8534°
Arg. of periapsis
200.2557°
True anomaly
159.8534°
Mean anomaly
159.8331°
Eccentric anomaly
159.84325°
Mean motion
3.15833 °/min
Orbital period
113.98 mins
BSTAR
0.000081993
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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 3 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. |
|---|---|---|---|---|---|---|---|
| 15 mins | 2025-11-07 10:26:19.042Z | 166.981° S | 2025-11-07 10:33:19.042Z | 98.883° ESE | 40.967° | 2025-11-07 10:41:19.042Z | 15.277° NNE |
| 12 mins | 2025-11-07 12:23:19.042Z | 240.493° WSW | 2025-11-07 12:29:19.042Z | 294.282° NW | 25.092° | 2025-11-07 12:35:19.042Z | 344.391° N |
| 11 mins | 2025-11-07 20:29:19.042Z | 24.845° NE | 2025-11-07 20:34:19.042Z | 68.532° E | 22.002° | 2025-11-07 20:40:19.042Z | 116.624° SE |
| 14 mins | 2025-11-07 22:23:19.042Z | 345.988° N | 2025-11-07 22:30:19.042Z | 246.332° WSW | 43.029° | 2025-11-07 22:37:19.042Z | 186.351° SSW |
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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