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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Edit Public Description
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: 18 hours ago
TLE from 18 hours ago
0 GONETS D1 1
1 23787U 96009A 25309.17203464 .00000008 00000-0 -17131-4 0 9993
2 23787 82.5748 82.3500 0011255 186.9588 346.6991 12.64100311371008Epoch: 2025-11-05T04:07Z
TLE epoch observation values (Epoch: 2025-11-05T04:07:43.792Z)
Latitude
6.24559°
Longitude
154.95583°
Altitude
1,399.68 km
Speed
7.164 km/s
True Right ascension
17h 26m 08s
True Declination
6° 12' 42"
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
17:53:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,412.142 km
Perigee altitude
1,394.626 km
Semi-major axis
7,781.521 km
Eccentricity
0.00113
Inclination
82.5748°
RAAN
82.35°
Arg. of periapsis
186.9588°
True anomaly
346.66939°
Mean anomaly
346.6991°
Eccentric anomaly
346.68425°
Mean motion
3.16189 °/min
Orbital period
113.86 mins
BSTAR
-0.000017131
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-11-05 22:52:21.980Z | 312.922° NW | 2025-11-05 22:56:21.980Z | 282.343° WNW | 15.356° | 2025-11-05 23:00:21.980Z | 251.853° W |
| 7 mins | 2025-11-06 07:52:21.980Z | 102.576° ESE | 2025-11-06 07:55:21.980Z | 78.698° E | 16.033° | 2025-11-06 07:59:21.980Z | 47.634° ENE |
| 15 mins | 2025-11-06 09:42:21.980Z | 185.863° SSW | 2025-11-06 09:49:21.980Z | 355.106° N | 44.904° | 2025-11-06 09:57:21.980Z | 7.588° NNE |
| 8 mins | 2025-11-06 11:41:21.980Z | 266.667° W | 2025-11-06 11:45:21.980Z | 298.869° NW | 16.768° | 2025-11-06 11:49:21.980Z | 330.187° NNW |
| 13 mins | 2025-11-06 19:43:21.980Z | 12.728° NNE | 2025-11-06 19:49:21.980Z | 69.433° E | 30.805° | 2025-11-06 19:56:21.980Z | 134.98° SE |
| 13 mins | 2025-11-06 21:38:21.980Z | 335.614° NNW | 2025-11-06 21:44:21.980Z | 274.28° WNW | 35.429° | 2025-11-06 21:51:21.980Z | 205.065° SW |
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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