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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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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 GONETS D1 3
1 23789U 96009C 26265.91038288 .00000041 00000-0 16838-3 0 9997
2 23789 82.5737 257.4402 0004894 190.4104 169.6887 12.62688052409986Epoch: 2026-09-22T21:50Z
TLE epoch observation values (Epoch: 2026-09-22T21:50:57.080Z)
Latitude
-0.00001°
Longitude
-72.06672°
Altitude
1,418.351 km
Speed
7.15 km/s
True Right ascension
17h 09m 45s
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
06:09:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,413 km
Perigee altitude
1,405.378 km
Semi-major axis
7,787.326 km
Eccentricity
0.00049
Inclination
82.5737°
RAAN
257.4402°
Arg. of periapsis
190.4104°
True anomaly
169.69873°
Mean anomaly
169.6887°
Eccentric anomaly
169.69372°
Mean motion
3.15835 °/min
Orbital period
113.98 mins
BSTAR
0.00016838
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-09-23 22:42:02.302Z | 123.171° SE | 2026-09-23 22:47:02.302Z | 81.738° E | 23.223° | 2026-09-23 22:53:02.302Z | 34.294° NE |
| 15 mins | 2026-09-24 00:34:02.302Z | 197.755° SSW | 2026-09-24 00:41:02.302Z | 269.955° W | 69.249° | 2026-09-24 00:49:02.302Z | 2.52° NNE |
| 5 mins | 2026-09-24 02:36:02.302Z | 287.1° WNW | 2026-09-24 02:38:02.302Z | 301.993° NW | 12.637° | 2026-09-24 02:41:02.302Z | 323.701° NNW |
| 14 mins | 2026-09-24 10:36:02.302Z | 6.722° NNE | 2026-09-24 10:43:02.302Z | 84.805° E | 48.636° | 2026-09-24 10:50:02.302Z | 148.107° SSE |
| 13 mins | 2026-09-24 12:31:02.302Z | 331.114° NNW | 2026-09-24 12:37:02.302Z | 277.98° WNW | 33.848° | 2026-09-24 12:44:02.302Z | 216.292° SW |
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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