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: 10 hours ago
TLE from 10 hours ago
0 GONETS D1 3
1 23789U 96009C 25324.74288712 .00000014 00000-0 17916-4 0 9991
2 23789 82.5773 92.9475 0005701 168.9369 191.1848 12.62679184371340Epoch: 2025-11-20T17:49Z
TLE epoch observation values (Epoch: 2025-11-20T17:49:45.447Z)
Latitude
-0.00007°
Longitude
125.51223°
Altitude
1,418.993 km
Speed
7.149 km/s
True Right ascension
06h 11m 47s
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
00:34:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,413.665 km
Perigee altitude
1,404.786 km
Semi-major axis
7,787.363 km
Eccentricity
0.00057
Inclination
82.5773°
RAAN
92.9475°
Arg. of periapsis
168.9369°
True anomaly
191.17214°
Mean anomaly
191.1848°
Eccentric anomaly
191.17847°
Mean motion
3.15833 °/min
Orbital period
113.98 mins
BSTAR
0.000017916
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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 | 2025-11-21 09:08:19.783Z | 173.91° S | 2025-11-21 09:15:19.783Z | 87.877° E | 43.514° | 2025-11-21 09:23:19.783Z | 11.975° NNE |
| 10 mins | 2025-11-21 11:06:19.783Z | 252.889° W | 2025-11-21 11:11:19.783Z | 296.95° NW | 21.588° | 2025-11-21 11:16:19.783Z | 338.09° N |
| 12 mins | 2025-11-21 19:10:19.783Z | 18.108° NNE | 2025-11-21 19:16:19.783Z | 72.144° E | 25.453° | 2025-11-21 19:22:19.783Z | 123.069° SE |
| 14 mins | 2025-11-21 21:05:19.783Z | 341.222° N | 2025-11-21 21:11:19.783Z | 274.613° WNW | 40.588° | 2025-11-21 21:19:19.783Z | 192.824° SSW |
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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