GONETS D1 1, 23787
Orbit data source: Space-Track
GONETS D1 1, 23787 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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23787 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: 20 hours ago
TLE from 20 hours ago
0 GONETS D1 1
1 23787U 96009A 26265.66661738 .00000030 00000-0 10775-3 0 9991
2 23787 82.5740 236.4596 0011052 174.5569 359.1303 12.64109131411622Epoch: 2026-09-22T15:59Z
TLE epoch observation values (Epoch: 2026-09-22T15:59:55.741Z)
Latitude
6.18864°
Longitude
174.14274°
Altitude
1,399.571 km
Speed
7.165 km/s
True Right ascension
03h 42m 36s
True Declination
6° 09' 18"
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
04:55:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,411.948 km
Perigee altitude
1,394.748 km
Semi-major axis
7,781.485 km
Eccentricity
0.00111
Inclination
82.574°
RAAN
236.4596°
Arg. of periapsis
174.5569°
True anomaly
359.12838°
Mean anomaly
359.1303°
Eccentric anomaly
359.12934°
Mean motion
3.16191 °/min
Orbital period
113.86 mins
BSTAR
0.00010775
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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 1 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. |
|---|---|---|---|---|---|---|---|
| 13 mins | 2026-09-23 21:34:31.783Z | 140.202° SSE | 2026-09-23 21:41:31.783Z | 80.417° E | 30.794° | 2026-09-23 21:47:31.783Z | 29.808° NE |
| 15 mins | 2026-09-23 23:28:31.783Z | 209.086° SW | 2026-09-23 23:35:31.783Z | 280.567° WNW | 53.716° | 2026-09-23 23:43:31.783Z | 358.57° N |
| 14 mins | 2026-09-24 09:29:31.783Z | 1.173° NNE | 2026-09-24 09:36:31.783Z | 86.35° E | 62.58° | 2026-09-24 09:43:31.783Z | 157.936° S |
| 11 mins | 2026-09-24 11:25:31.783Z | 321.455° NNW | 2026-09-24 11:30:31.783Z | 277.182° WNW | 25.765° | 2026-09-24 11:36:31.783Z | 228.074° WSW |
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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