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: 5 hours ago
TLE from 5 hours ago
0 GONETS D1 2
1 23788U 96009B 26086.83863108 .00000014 00000-0 19381-4 0 9992
2 23788 82.5761 356.5523 0005900 253.9035 106.1407 12.63213966387825Epoch: 2026-03-27T20:07Z
TLE epoch observation values (Epoch: 2026-03-27T20:07:37.725Z)
Latitude
-0.00003°
Longitude
-130.62237°
Altitude
1,413.718 km
Speed
7.153 km/s
True Right ascension
23h 46m 12s
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
06:28:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,411.619 km
Perigee altitude
1,402.433 km
Semi-major axis
7,785.163 km
Eccentricity
0.00059
Inclination
82.5761°
RAAN
356.5523°
Arg. of periapsis
253.9035°
True anomaly
106.20563°
Mean anomaly
106.1407°
Eccentric anomaly
106.17317°
Mean motion
3.15967 °/min
Orbital period
113.94 mins
BSTAR
0.000019381
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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 | 2026-03-28 04:20:31.854Z | 16.797° NNE | 2026-03-28 04:26:31.854Z | 66.035° ENE | 23.437° | 2026-03-28 04:32:31.854Z | 117.314° SE |
| 14 mins | 2026-03-28 06:15:31.854Z | 344.633° N | 2026-03-28 06:22:31.854Z | 257.161° W | 42.222° | 2026-03-28 06:29:31.854Z | 189.55° SSW |
| 10 mins | 2026-03-28 17:10:31.854Z | 121.829° SE | 2026-03-28 17:15:31.854Z | 76.586° E | 22.675° | 2026-03-28 17:20:31.854Z | 35.963° NE |
| 14 mins | 2026-03-28 19:02:31.854Z | 201.408° SSW | 2026-03-28 19:09:31.854Z | 292.099° WNW | 42.17° | 2026-03-28 19:16:31.854Z | 0.646° NNE |
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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