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: 1 day ago
TLE from 1 day ago
0 GONETS D1 5
1 24729U 97006E 25259.93785707 .00000040 00000-0 16181-3 0 9999
2 24729 82.5962 56.6717 0004848 142.9585 333.1542 12.62977572317963Epoch: 2025-09-16T22:30Z
TLE epoch observation values (Epoch: 2025-09-16T22:30:30.85Z)
Latitude
63.03737°
Longitude
-111.80292°
Altitude
1,418.106 km
Speed
7.159 km/s
True Right ascension
14h 47m 47s
True Declination
62° 54' 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
16:48:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,411.772 km
Perigee altitude
1,404.223 km
Semi-major axis
7,786.135 km
Eccentricity
0.00048
Inclination
82.5962°
RAAN
56.6717°
Arg. of periapsis
142.9585°
True anomaly
333.1291°
Mean anomaly
333.1542°
Eccentric anomaly
333.14165°
Mean motion
3.15908 °/min
Orbital period
113.96 mins
BSTAR
0.00016181
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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. |
|---|---|---|---|---|---|---|---|
| 14 mins | 2025-09-18 10:06:48.177Z | 147.451° SSE | 2025-09-18 10:13:48.177Z | 86.368° E | 30.881° | 2025-09-18 10:20:48.177Z | 24.832° NE |
| 14 mins | 2025-09-18 12:01:48.177Z | 217.058° SW | 2025-09-18 12:08:48.177Z | 289.503° WNW | 35.359° | 2025-09-18 12:15:48.177Z | 354.249° N |
| 6 mins | 2025-09-18 20:10:48.177Z | 41.835° NE | 2025-09-18 20:12:48.177Z | 57.013° ENE | 13.295° | 2025-09-18 20:16:48.177Z | 86.779° E |
| 15 mins | 2025-09-18 22:02:48.177Z | 357.282° N | 2025-09-18 22:09:48.177Z | 88.249° E | 43.916° | 2025-09-18 22:17:48.177Z | 166.415° S |
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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