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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 GONETS D1 8
1 27059U 01058E 26068.97574813 -.00000160 00000-0 -96122-3 0 9995
2 27059 82.5366 276.2869 0002842 105.4892 254.6512 12.61553802114060Epoch: 2026-03-09T23:25Z
TLE epoch observation values (Epoch: 2026-03-09T23:25:04.638Z)
Latitude
-0.00007°
Longitude
117.35659°
Altitude
1,419.852 km
Speed
7.151 km/s
True Right ascension
18h 25m 08s
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
11:08:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,416.075 km
Perigee altitude
1,411.646 km
Semi-major axis
7,791.998 km
Eccentricity
0.00028
Inclination
82.5366°
RAAN
276.2869°
Arg. of periapsis
105.4892°
True anomaly
254.6198°
Mean anomaly
254.6512°
Eccentric anomaly
254.6355°
Mean motion
3.15551 °/min
Orbital period
114.09 mins
BSTAR
-0.00096122
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-03-10 12:52:14.748Z | 121.73° SE | 2026-03-10 12:57:14.748Z | 81.988° E | 20.062° | 2026-03-10 13:02:14.748Z | 40.9° NE |
| 15 mins | 2026-03-10 14:44:14.748Z | 194.769° SSW | 2026-03-10 14:51:14.748Z | 259.608° W | 43.744° | 2026-03-10 14:59:14.748Z | 3.63° NNE |
| 5 mins | 2026-03-10 16:46:14.748Z | 284.932° WNW | 2026-03-10 16:48:14.748Z | 300.243° NW | 13.32° | 2026-03-10 16:51:14.748Z | 322.677° NNW |
| 14 mins | 2026-03-11 00:47:14.748Z | 9.248° NNE | 2026-03-11 00:53:14.748Z | 72.298° E | 35.893° | 2026-03-11 01:01:14.748Z | 147.112° SSE |
| 13 mins | 2026-03-11 02:42:14.748Z | 330.803° NNW | 2026-03-11 02:48:14.748Z | 274.06° WNW | 30.372° | 2026-03-11 02:55:14.748Z | 213.419° SW |
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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