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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 GONETS D1 2
1 23788U 96009B 26194.71251031 .00000018 00000-0 39391-4 0 9992
2 23788 82.5712 287.5243 0006995 19.3368 340.7988 12.63217491401443Epoch: 2026-07-13T17:06Z
TLE epoch observation values (Epoch: 2026-07-13T17:06:00.890Z)
Latitude
-0.00001°
Longitude
99.4275°
Altitude
1,407.278 km
Speed
7.159 km/s
True Right ascension
19h 10m 05s
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
17:39:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,412.458 km
Perigee altitude
1,401.566 km
Semi-major axis
7,785.149 km
Eccentricity
0.0007
Inclination
82.5712°
RAAN
287.5243°
Arg. of periapsis
19.3368°
True anomaly
340.77242°
Mean anomaly
340.7988°
Eccentric anomaly
340.78561°
Mean motion
3.15968 °/min
Orbital period
113.94 mins
BSTAR
0.000039391
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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. |
|---|---|---|---|---|---|---|---|
| 15 mins | 2026-07-14 06:29:09.195Z | 168.934° S | 2026-07-14 06:37:09.195Z | 85.894° E | 41.33° | 2026-07-14 06:44:09.195Z | 15.804° NNE |
| 12 mins | 2026-07-14 08:27:09.195Z | 243.649° WSW | 2026-07-14 08:32:09.195Z | 288.105° WNW | 24.523° | 2026-07-14 08:39:09.195Z | 346.379° N |
| 11 mins | 2026-07-14 16:32:09.195Z | 22.659° NE | 2026-07-14 16:37:09.195Z | 65.288° ENE | 22.391° | 2026-07-14 16:43:09.195Z | 115.443° SE |
| 15 mins | 2026-07-14 18:26:09.195Z | 345.925° N | 2026-07-14 18:33:09.195Z | 258.854° W | 43.003° | 2026-07-14 18:41:09.195Z | 186.289° 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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