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: 12 hours ago
TLE from 12 hours ago
0 GONETS D1 2
1 23788U 96009B 26139.98360325 .00000021 00000-0 57139-4 0 9991
2 23788 82.5691 322.5485 0007787 128.7225 231.4563 12.63216271394535Epoch: 2026-05-19T23:36Z
TLE epoch observation values (Epoch: 2026-05-19T23:36:23.320Z)
Latitude
-0.00012°
Longitude
90.80164°
Altitude
1,416.21 km
Speed
7.151 km/s
True Right ascension
21h 30m 11s
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
20:28:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,413.079 km
Perigee altitude
1,400.955 km
Semi-major axis
7,785.154 km
Eccentricity
0.00078
Inclination
82.5691°
RAAN
322.5485°
Arg. of periapsis
128.7225°
True anomaly
231.38655°
Mean anomaly
231.4563°
Eccentric anomaly
231.42142°
Mean motion
3.15967 °/min
Orbital period
113.94 mins
BSTAR
0.000057139
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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. |
|---|---|---|---|---|---|---|---|
| 16 mins | 2026-05-20 12:59:51.450Z | 188.78° SSW | 2026-05-20 13:07:51.450Z | 317.822° NNW | 44.692° | 2026-05-20 13:15:51.450Z | 6.433° NNE |
| 7 mins | 2026-05-20 15:00:51.450Z | 274.632° WNW | 2026-05-20 15:03:51.450Z | 298.574° NW | 15.448° | 2026-05-20 15:07:51.450Z | 329.249° NNW |
| 14 mins | 2026-05-20 23:01:51.450Z | 9.86° NNE | 2026-05-20 23:08:51.450Z | 79.858° E | 32.516° | 2026-05-20 23:15:51.450Z | 140.208° SSE |
| 14 mins | 2026-05-21 00:56:51.450Z | 335.432° NNW | 2026-05-21 01:02:51.450Z | 281.055° WNW | 33.485° | 2026-05-21 01:10:51.450Z | 206.256° 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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