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: 11 hours ago
TLE from 11 hours ago
0 GONETS D1 3
1 23789U 96009C 26049.99279596 .00000004 00000-0 -36185-4 0 9992
2 23789 82.5779 35.3071 0005031 346.3308 13.7646 12.62682343382731Epoch: 2026-02-18T23:49Z
TLE epoch observation values (Epoch: 2026-02-18T23:49:37.570Z)
Latitude
-0.00007°
Longitude
-111.04993°
Altitude
1,410.816 km
Speed
7.157 km/s
True Right ascension
02h 21m 13s
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
13:42:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,413.131 km
Perigee altitude
1,405.295 km
Semi-major axis
7,787.35 km
Eccentricity
0.0005
Inclination
82.5779°
RAAN
35.3071°
Arg. of periapsis
346.3308°
True anomaly
13.77833°
Mean anomaly
13.7646°
Eccentric anomaly
13.77146°
Mean motion
3.15834 °/min
Orbital period
113.98 mins
BSTAR
-0.000036185
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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. |
|---|---|---|---|---|---|---|---|
| 13 mins | 2026-02-19 11:52:03.169Z | 334.034° NNW | 2026-02-19 11:58:03.169Z | 281.114° WNW | 31.784° | 2026-02-19 12:05:03.169Z | 212.794° SW |
| 14 mins | 2026-02-19 22:45:03.169Z | 151.158° SSE | 2026-02-19 22:51:03.169Z | 94.675° ESE | 34.238° | 2026-02-19 22:59:03.169Z | 20.696° NNE |
| 14 mins | 2026-02-20 00:40:03.169Z | 224.826° SW | 2026-02-20 00:46:03.169Z | 280.98° WNW | 31.958° | 2026-02-20 00:54:03.169Z | 353.489° N |
| 8 mins | 2026-02-20 08:48:03.169Z | 35.896° NE | 2026-02-20 08:51:03.169Z | 59.662° ENE | 16.04° | 2026-02-20 08:56:03.169Z | 97.918° ESE |
| 4 mins | 2026-02-20 10:41:03.169Z | 353.892° N | 2026-02-20 10:45:03.169Z | 357.848° N | 37.734° | 2026-02-20 10:45:03.169Z | 357.848° N |
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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