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: 19 hours ago
TLE from 19 hours ago
0 GONETS D1 3
1 23789U 96009C 25309.13334374 .00000019 00000-0 47540-4 0 9994
2 23789 82.5751 102.9163 0005073 203.8636 156.2221 12.62678306369372Epoch: 2025-11-05T03:12Z
TLE epoch observation values (Epoch: 2025-11-05T03:12:00.899Z)
Latitude
0.00002°
Longitude
10.30217°
Altitude
1,418.257 km
Speed
7.15 km/s
True Right ascension
06h 51m 39s
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
17:53:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,413.18 km
Perigee altitude
1,405.279 km
Semi-major axis
7,787.366 km
Eccentricity
0.00051
Inclination
82.5751°
RAAN
102.9163°
Arg. of periapsis
203.8636°
True anomaly
156.24552°
Mean anomaly
156.2221°
Eccentric anomaly
156.23381°
Mean motion
3.15833 °/min
Orbital period
113.98 mins
BSTAR
0.00004754
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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 | 2025-11-05 22:49:45.784Z | 343.606° N | 2025-11-05 22:57:45.784Z | 259.338° W | 39.882° | 2025-11-05 23:04:45.784Z | 195.021° SSW |
| 12 mins | 2025-11-06 09:44:45.784Z | 133.11° SE | 2025-11-06 09:50:45.784Z | 78.985° E | 25.775° | 2025-11-06 09:56:45.784Z | 30.162° NE |
| 15 mins | 2025-11-06 11:37:45.784Z | 206.756° SW | 2025-11-06 11:44:45.784Z | 280.527° WNW | 39.957° | 2025-11-06 11:52:45.784Z | 359.524° N |
| 13 mins | 2025-11-06 21:39:45.784Z | 3.084° NNE | 2025-11-06 21:45:45.784Z | 65.739° ENE | 40.714° | 2025-11-06 21:52:45.784Z | 154.472° SSE |
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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