GONETS D1 8, 27059
Orbit data source: Space-Track
GONETS D1 8, 27059 is a payload satellite owned by Gonets (CIS) in LEO that was launched on Fri, 28 Dec 2001 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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27059 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: 7 hours ago
TLE from 7 hours ago
0 GONETS D1 8
1 27059U 01058E 26227.19245973 -.00000044 00000-0 -30981-3 0 9990
2 27059 82.5439 174.9718 0003197 100.1823 259.9629 12.61557366134011Epoch: 2026-08-15T04:37Z
TLE epoch observation values (Epoch: 2026-08-15T04:37:08.520Z)
Latitude
0.00004°
Longitude
142.07944°
Altitude
1,419.686 km
Speed
7.151 km/s
True Right ascension
11h 39m 53s
True Declination
0° 00' 00"
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
02:11:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,416.337 km
Perigee altitude
1,411.355 km
Semi-major axis
7,791.983 km
Eccentricity
0.00032
Inclination
82.5439°
RAAN
174.9718°
Arg. of periapsis
100.1823°
True anomaly
259.92683°
Mean anomaly
259.9629°
Eccentric anomaly
259.94486°
Mean motion
3.15552 °/min
Orbital period
114.09 mins
BSTAR
-0.00030981
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Other satellites on launch #58 in the year 2001 (2001-12-28 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 8 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 | 2026-08-15 19:57:12.726Z | 134.97° SE | 2026-08-15 20:03:12.726Z | 86.661° E | 24.75° | 2026-08-15 20:09:12.726Z | 34.095° NE |
| 15 mins | 2026-08-15 21:51:12.726Z | 205.455° SW | 2026-08-15 21:58:12.726Z | 287.534° WNW | 40.722° | 2026-08-15 22:06:12.726Z | 0.765° NNE |
| 14 mins | 2026-08-16 07:53:12.726Z | 3.105° NNE | 2026-08-16 08:00:12.726Z | 87.193° E | 40.211° | 2026-08-16 08:07:12.726Z | 154.662° SSE |
| 11 mins | 2026-08-16 09:49:12.726Z | 323.62° NNW | 2026-08-16 09:54:12.726Z | 278.98° WNW | 25.348° | 2026-08-16 10:00:12.726Z | 226.628° WSW |
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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