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: 1 day ago
TLE from 1 day ago
0 GONETS D1 3
1 23789U 96009C 25261.11611878 .00000031 00000-0 11225-3 0 9990
2 23789 82.5783 133.5846 0005100 331.9089 28.1726 12.62675370363314Epoch: 2025-09-18T02:47Z
TLE epoch observation values (Epoch: 2025-09-18T02:47:12.662Z)
Latitude
-0.00007°
Longitude
94.4995°
Altitude
1,411.149 km
Speed
7.156 km/s
True Right ascension
08h 54m 20s
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
20:52:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,413.213 km
Perigee altitude
1,405.27 km
Semi-major axis
7,787.378 km
Eccentricity
0.00051
Inclination
82.5783°
RAAN
133.5846°
Arg. of periapsis
331.9089°
True anomaly
28.20021°
Mean anomaly
28.1726°
Eccentric anomaly
28.1864°
Mean motion
3.15832 °/min
Orbital period
113.98 mins
BSTAR
0.00011225
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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 | 2025-09-19 04:07:06.813Z | 342.244° N | 2025-09-19 04:15:06.813Z | 265.163° W | 38.057° | 2025-09-19 04:22:06.813Z | 199.378° SSW |
| 12 mins | 2025-09-19 15:02:06.813Z | 137.195° SSE | 2025-09-19 15:08:06.813Z | 80.791° E | 27.962° | 2025-09-19 15:14:06.813Z | 29.273° NE |
| 14 mins | 2025-09-19 16:56:06.813Z | 213.334° SW | 2025-09-19 17:02:06.813Z | 276.857° WNW | 37.951° | 2025-09-19 17:10:06.813Z | 357.508° N |
| 14 mins | 2025-09-20 02:57:06.813Z | 0.393° NNE | 2025-09-20 03:04:06.813Z | 93.817° ESE | 42.339° | 2025-09-20 03:11:06.813Z | 160.422° S |
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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