GONETS D1 5, 24729
Orbit data source: Space-Track
GONETS D1 5, 24729 is a payload satellite owned by Gonets (CIS) in LEO that was launched on Fri, 14 Feb 1997 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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24729 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: 7 hours ago
TLE from 7 hours ago
0 GONETS D1 5
1 24729U 97006E 25308.17015411 .00000021 00000-0 56724-4 0 9995
2 24729 82.6030 25.9463 0004918 54.9059 10.6466 12.62979668324051Epoch: 2025-11-04T04:05Z
TLE epoch observation values (Epoch: 2025-11-04T04:05:01.315Z)
Latitude
64.61545°
Longitude
-63.1721°
Altitude
1,418.017 km
Speed
7.159 km/s
True Right ascension
02h 46m 58s
True Declination
64° 29' 36"
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
06:55:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,411.818 km
Perigee altitude
1,404.159 km
Semi-major axis
7,786.126 km
Eccentricity
0.00049
Inclination
82.603°
RAAN
25.9463°
Arg. of periapsis
54.9059°
True anomaly
10.65702°
Mean anomaly
10.6466°
Eccentric anomaly
10.65181°
Mean motion
3.15908 °/min
Orbital period
113.96 mins
BSTAR
0.000056724
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Other satellites on launch #6 in the year 1997 (1997-02-14 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 5 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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2025-11-04 15:45:50.220Z | 18.866° NNE | 2025-11-04 15:51:50.220Z | 71.024° E | 23.881° | 2025-11-04 15:57:50.220Z | 120.37° SE |
| 14 mins | 2025-11-04 17:40:50.220Z | 343.302° N | 2025-11-04 17:46:50.220Z | 278.032° WNW | 41.854° | 2025-11-04 17:54:50.220Z | 189.914° SSW |
| 11 mins | 2025-11-05 04:34:50.220Z | 127.09° SE | 2025-11-05 04:39:50.220Z | 84.445° E | 23.286° | 2025-11-05 04:45:50.220Z | 34.08° NE |
| 14 mins | 2025-11-05 06:27:50.220Z | 203.197° SW | 2025-11-05 06:33:50.220Z | 264.835° W | 41.587° | 2025-11-05 06:41:50.220Z | 0.54° NNE |
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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