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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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Identifier
23787, 1996-009A
Orbit
LEO
Country
Flag of CISCIS
Related 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)
Icon of a cake. It is the launch day of the satellite!1996-02-19 (30 years ago)
Launch vehicle
TSIKLON-3
Launch site
Plesetsk Missile And Space Complex (PKMTR)
Object type
Payload
Rocket body
Debris
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 & history
Last TLE update: 6 hours ago

TLE from 6 hours ago
0 GONETS D1 1
1 23787U 96009A   26050.29577124  .00000008  00000-0 -12809-4 0  9994
2 23787  82.5795  14.3824 0010458 316.1596 160.7899 12.64103767384413
Epoch: 2026-02-19T07:05Z
TLE epoch observation values (Epoch: 2026-02-19T07:05:54.635Z)
Latitude
62.16901°
Longitude
-75.55479°
Altitude
1,424.36 km
Speed
7.151 km/s
True Right ascension
12h 00m 41s
True Declination
62° 02' 20"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
15:44:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,411.508 km
Perigee altitude
1,395.232 km
Semi-major axis
7,781.507 km
Eccentricity
0.00105
Inclination
82.5795°
RAAN
14.3824°
Arg. of periapsis
316.1596°
True anomaly
160.82928°
Mean anomaly
160.7899°
Eccentric anomaly
160.8096°
Mean motion
3.1619 °/min
Orbital period
113.86 mins
BSTAR
-0.000012809
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