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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 GONETS D1 5
1 24729U 97006E 26308.05603307 .00000019 00000-0 44760-4 0 9994
2 24729 82.5974 153.4785 0003635 302.8608 178.6441 12.62989163370118Epoch: 2026-11-04T01:20Z
TLE epoch observation values (Epoch: 2026-11-04T01:20:41.257Z)
Latitude
57.81366°
Longitude
-101.85648°
Altitude
1,423.142 km
Speed
7.153 km/s
True Right ascension
21h 26m 30s
True Declination
57° 40' 18"
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
11:11:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,410.78 km
Perigee altitude
1,405.12 km
Semi-major axis
7,786.087 km
Eccentricity
0.00036
Inclination
82.5974°
RAAN
153.4785°
Arg. of periapsis
302.8608°
True anomaly
178.64509°
Mean anomaly
178.6441°
Eccentric anomaly
178.64459°
Mean motion
3.15911 °/min
Orbital period
113.96 mins
BSTAR
0.00004476
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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. |
|---|---|---|---|---|---|---|---|
| 13 mins | 2026-11-04 16:02:25.433Z | 237.639° WSW | 2026-11-04 16:08:25.433Z | 287.165° WNW | 27.532° | 2026-11-04 16:15:25.433Z | 345.983° N |
| 11 mins | 2026-11-05 00:08:25.433Z | 21.463° NNE | 2026-11-05 00:13:25.433Z | 62.789° ENE | 24.065° | 2026-11-05 00:19:25.433Z | 113.795° SE |
| 15 mins | 2026-11-05 02:02:25.433Z | 346.53° N | 2026-11-05 02:09:25.433Z | 271.126° WNW | 69.76° | 2026-11-05 02:17:25.433Z | 186.202° SSW |
| 11 mins | 2026-11-05 12:57:25.433Z | 122.938° SE | 2026-11-05 13:02:25.433Z | 81.103° E | 23.28° | 2026-11-05 13:08:25.433Z | 33.882° NE |
| 15 mins | 2026-11-05 14:49:25.433Z | 198.03° SSW | 2026-11-05 14:56:25.433Z | 274.16° WNW | 69.118° | 2026-11-05 15:04:25.433Z | 2.555° 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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