GONETS D1 2, 23788
Orbit data source: Space-Track
GONETS D1 2, 23788 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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23788 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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 GONETS D1 2
1 23788U 96009B 26050.00938365 .00000009 00000-0 -76778-5 0 9999
2 23788 82.5721 20.1069 0006824 347.8518 12.2408 12.63213035383174Epoch: 2026-02-19T00:13Z
TLE epoch observation values (Epoch: 2026-02-19T00:13:30.747Z)
Latitude
-0.00001°
Longitude
-132.23804°
Altitude
1,407.247 km
Speed
7.159 km/s
True Right ascension
01h 20m 25s
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
15:45:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,412.343 km
Perigee altitude
1,401.718 km
Semi-major axis
7,785.167 km
Eccentricity
0.00068
Inclination
82.5721°
RAAN
20.1069°
Arg. of periapsis
347.8518°
True anomaly
12.25739°
Mean anomaly
12.2408°
Eccentric anomaly
12.2491°
Mean motion
3.15967 °/min
Orbital period
113.94 mins
BSTAR
-0.0000076778
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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 2 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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2026-02-19 21:14:40.809Z | 134.151° SE | 2026-02-19 21:20:40.809Z | 84.725° E | 24.632° | 2026-02-19 21:26:40.809Z | 33.208° NE |
| 14 mins | 2026-02-19 23:08:40.809Z | 206.009° SW | 2026-02-19 23:14:40.809Z | 267.192° W | 40.567° | 2026-02-19 23:22:40.809Z | 359.471° N |
| 14 mins | 2026-02-20 09:09:40.809Z | 3.78° NNE | 2026-02-20 09:16:40.809Z | 89.191° E | 39.818° | 2026-02-20 09:23:40.809Z | 154.163° SSE |
| 11 mins | 2026-02-20 11:05:40.809Z | 322.628° NNW | 2026-02-20 11:10:40.809Z | 276.208° WNW | 25.805° | 2026-02-20 11:16:40.809Z | 224.888° SW |
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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