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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 GONETS D1 1
1 23787U 96009A 26124.52311731 .00000027 00000-0 90042-4 0 9997
2 23787 82.5762 326.8659 0011755 138.1252 282.2232 12.64106424393791Epoch: 2026-05-04T12:33Z
TLE epoch observation values (Epoch: 2026-05-04T12:33:17.335Z)
Latitude
59.47678°
Longitude
-71.16376°
Altitude
1,414.16 km
Speed
7.16 km/s
True Right ascension
22h 38m 16s
True Declination
59° 20' 20"
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
03:49:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,412.506 km
Perigee altitude
1,394.212 km
Semi-major axis
7,781.496 km
Eccentricity
0.00118
Inclination
82.5762°
RAAN
326.8659°
Arg. of periapsis
138.1252°
True anomaly
282.09151°
Mean anomaly
282.2232°
Eccentric anomaly
282.15736°
Mean motion
3.1619 °/min
Orbital period
113.86 mins
BSTAR
0.000090042
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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. |
|---|---|---|---|---|---|---|---|
| 14 mins | 2026-05-05 00:14:32.988Z | 10.648° NNE | 2026-05-05 00:21:32.988Z | 75.005° E | 29.926° | 2026-05-05 00:28:32.988Z | 135.17° SSE |
| 13 mins | 2026-05-05 02:10:32.988Z | 335.076° NNW | 2026-05-05 02:16:32.988Z | 266.696° W | 36.232° | 2026-05-05 02:23:32.988Z | 202.455° SSW |
| 13 mins | 2026-05-05 13:02:32.988Z | 141.274° SSE | 2026-05-05 13:08:32.988Z | 85.492° E | 29.556° | 2026-05-05 13:15:32.988Z | 25.526° NE |
| 14 mins | 2026-05-05 14:56:32.988Z | 215.369° SW | 2026-05-05 15:03:32.988Z | 293.245° NW | 36.412° | 2026-05-05 15:10:32.988Z | 355.777° N |
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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