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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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: 15 hours ago
TLE from 15 hours ago
0 GONETS D1 5
1 24729U 97006E 26127.91690089 .00000038 00000-0 15180-3 0 9995
2 24729 82.5965 268.2235 0003822 356.1569 125.4349 12.62986489347376Epoch: 2026-05-07T22:00Z
TLE epoch observation values (Epoch: 2026-05-07T22:00:20.236Z)
Latitude
57.6956°
Longitude
-119.41691°
Altitude
1,422.023 km
Speed
7.154 km/s
True Right ascension
05h 05m 41s
True Declination
57° 33' 12"
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
20:51:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,410.937 km
Perigee altitude
1,404.985 km
Semi-major axis
7,786.098 km
Eccentricity
0.00038
Inclination
82.5965°
RAAN
268.2235°
Arg. of periapsis
356.1569°
True anomaly
125.47057°
Mean anomaly
125.4349°
Eccentric anomaly
125.45274°
Mean motion
3.1591 °/min
Orbital period
113.96 mins
BSTAR
0.0001518
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-05-08 18:55:34.986Z | 40.831° NE | 2026-05-08 18:57:34.986Z | 55.184° ENE | 11.357° | 2026-05-08 18:59:34.986Z | 69.815° E |
| 15 mins | 2026-05-08 20:47:34.986Z | 359.619° N | 2026-05-08 20:54:34.986Z | 74.634° E | 42.327° | 2026-05-08 21:02:34.986Z | 160.897° S |
| 10 mins | 2026-05-08 22:44:34.986Z | 317.072° NNW | 2026-05-08 22:48:34.986Z | 281.711° WNW | 22.62° | 2026-05-08 22:54:34.986Z | 231.59° WSW |
| 14 mins | 2026-05-09 09:35:34.986Z | 169.082° S | 2026-05-09 09:41:34.986Z | 102.581° ESE | 42.355° | 2026-05-09 09:49:34.986Z | 13.715° NNE |
| 11 mins | 2026-05-09 11:32:34.986Z | 248.733° W | 2026-05-09 11:37:34.986Z | 293.894° NW | 23.21° | 2026-05-09 11:43:34.986Z | 343.059° 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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