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: 9 hours ago
TLE from 9 hours ago
0 GONETS D1 1
1 23787U 96009A 25299.89894962 .00000032 00000-0 11950-3 0 9997
2 23787 82.5731 88.2897 0010871 208.6279 266.5166 12.64099868369832Epoch: 2025-10-26T21:34Z
TLE epoch observation values (Epoch: 2025-10-26T21:34:29.247Z)
Latitude
64.05161°
Longitude
-106.30015°
Altitude
1,417.592 km
Speed
7.157 km/s
True Right ascension
16h 51m 19s
True Declination
63° 55' 39"
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
02:18:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,411.845 km
Perigee altitude
1,394.927 km
Semi-major axis
7,781.523 km
Eccentricity
0.00109
Inclination
82.5731°
RAAN
88.2897°
Arg. of periapsis
208.6279°
True anomaly
266.39227°
Mean anomaly
266.5166°
Eccentric anomaly
266.45443°
Mean motion
3.16189 °/min
Orbital period
113.86 mins
BSTAR
0.0001195
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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. |
|---|---|---|---|---|---|---|---|
| 15 mins | 2025-10-27 10:20:57.722Z | 170.711° S | 2025-10-27 10:28:57.722Z | 75.163° E | 42.036° | 2025-10-27 10:35:57.722Z | 14.326° NNE |
| 11 mins | 2025-10-27 12:18:57.722Z | 247.327° WSW | 2025-10-27 12:23:57.722Z | 291.97° WNW | 23.559° | 2025-10-27 12:29:57.722Z | 342.286° N |
| 11 mins | 2025-10-27 20:23:57.722Z | 25.917° NE | 2025-10-27 20:28:57.722Z | 72.198° E | 23.231° | 2025-10-27 20:34:57.722Z | 120.235° SE |
| 15 mins | 2025-10-27 22:16:57.722Z | 345.265° N | 2025-10-27 22:23:57.722Z | 270.527° WNW | 42.328° | 2025-10-27 22:31:57.722Z | 188.47° 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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