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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 GONETS D1 3
1 23789U 96009C 26194.36054919 .00000004 00000-0 -38009-4 0 9991
2 23789 82.5808 303.1360 0005294 18.7067 341.4218 12.62686462400951Epoch: 2026-07-13T08:39Z
TLE epoch observation values (Epoch: 2026-07-13T08:39:11.450Z)
Latitude
0.00001°
Longitude
-117.90788°
Altitude
1,410.696 km
Speed
7.157 km/s
True Right ascension
20h 12m 32s
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
15:56:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,413.318 km
Perigee altitude
1,405.073 km
Semi-major axis
7,787.333 km
Eccentricity
0.00053
Inclination
82.5808°
RAAN
303.136°
Arg. of periapsis
18.7067°
True anomaly
341.40246°
Mean anomaly
341.4218°
Eccentric anomaly
341.41213°
Mean motion
3.15835 °/min
Orbital period
113.98 mins
BSTAR
-0.000038009
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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. |
|---|---|---|---|---|---|---|---|
| 16 mins | 2026-07-14 07:33:09.740Z | 170.49° S | 2026-07-14 07:41:09.740Z | 86.252° E | 41.98° | 2026-07-14 07:49:09.740Z | 13.706° NNE |
| 12 mins | 2026-07-14 09:31:09.740Z | 244.345° WSW | 2026-07-14 09:36:09.740Z | 287.351° WNW | 23.711° | 2026-07-14 09:43:09.740Z | 345.444° N |
| 12 mins | 2026-07-14 17:36:09.740Z | 20.384° NNE | 2026-07-14 17:42:09.740Z | 72.876° E | 23.177° | 2026-07-14 17:48:09.740Z | 120.251° SE |
| 15 mins | 2026-07-14 19:30:09.740Z | 345.487° N | 2026-07-14 19:37:09.740Z | 273.172° WNW | 42.438° | 2026-07-14 19:45:09.740Z | 188.356° 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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