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: 12 hours ago
TLE from 12 hours ago
0 GONETS D1 3
1 23789U 96009C 25354.93187781 .00000033 00000-0 12706-3 0 9991
2 23789 82.5789 73.6728 0006422 108.8149 251.3640 12.62680237375157Epoch: 2025-12-20T22:21Z
TLE epoch observation values (Epoch: 2025-12-20T22:21:54.242Z)
Latitude
0.00003°
Longitude
8.4452°
Altitude
1,416.233 km
Speed
7.152 km/s
True Right ascension
04h 54m 41s
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
09:12:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,414.222 km
Perigee altitude
1,404.22 km
Semi-major axis
7,787.358 km
Eccentricity
0.00064
Inclination
82.5789°
RAAN
73.6728°
Arg. of periapsis
108.8149°
True anomaly
251.29429°
Mean anomaly
251.364°
Eccentric anomaly
251.32914°
Mean motion
3.15833 °/min
Orbital period
113.98 mins
BSTAR
0.00012706
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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. |
|---|---|---|---|---|---|---|---|
| 14 mins | 2025-12-21 16:04:47.513Z | 9.853° NNE | 2025-12-21 16:11:47.513Z | 68.256° E | 28.365° | 2025-12-21 16:18:47.513Z | 130.568° SE |
| 14 mins | 2025-12-21 18:00:47.513Z | 338.891° N | 2025-12-21 18:06:47.513Z | 280.359° WNW | 37.775° | 2025-12-21 18:14:47.513Z | 198.723° SSW |
| 12 mins | 2025-12-22 04:54:47.513Z | 135.907° SSE | 2025-12-22 04:59:47.513Z | 90.092° ESE | 28.01° | 2025-12-22 05:06:47.513Z | 27.971° NE |
| 15 mins | 2025-12-22 06:47:47.513Z | 211.284° SW | 2025-12-22 06:54:47.513Z | 283.32° WNW | 37.909° | 2025-12-22 07:02:47.513Z | 358.152° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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