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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 GONETS D1 3
1 23789U 96009C 26124.55382052 .00000037 00000-0 14448-3 0 9992
2 23789 82.5808 347.7150 0005541 153.8648 206.2724 12.62684826392146Epoch: 2026-05-04T13:17Z
TLE epoch observation values (Epoch: 2026-05-04T13:17:30.092Z)
Latitude
-0.00004°
Longitude
-74.10175°
Altitude
1,418.484 km
Speed
7.15 km/s
True Right ascension
23h 10m 51s
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
03:50:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,413.517 km
Perigee altitude
1,404.887 km
Semi-major axis
7,787.339 km
Eccentricity
0.00055
Inclination
82.5808°
RAAN
347.715°
Arg. of periapsis
153.8648°
True anomaly
206.24431°
Mean anomaly
206.2724°
Eccentric anomaly
206.25835°
Mean motion
3.15834 °/min
Orbital period
113.98 mins
BSTAR
0.00014448
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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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2026-05-05 01:19:00.519Z | 17.213° NNE | 2026-05-05 01:25:00.519Z | 68.372° E | 24.345° | 2026-05-05 01:31:00.519Z | 119.812° SE |
| 14 mins | 2026-05-05 03:14:00.519Z | 343.262° N | 2026-05-05 03:21:00.519Z | 252.914° W | 41.324° | 2026-05-05 03:28:00.519Z | 191.211° SSW |
| 11 mins | 2026-05-05 14:09:00.519Z | 124.167° SE | 2026-05-05 14:14:00.519Z | 78.009° E | 23.822° | 2026-05-05 14:20:00.519Z | 30.971° NE |
| 15 mins | 2026-05-05 16:01:00.519Z | 203.301° SW | 2026-05-05 16:08:00.519Z | 284.127° WNW | 41.455° | 2026-05-05 16:16:00.519Z | 1.166° NNE |
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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