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: 4 hours ago
TLE from 4 hours ago
0 GONETS D1 8
1 27059U 01058E 26276.99694904 .00000003 00000-0 -42408-4 0 9996
2 27059 82.5412 143.0992 0002662 23.9826 336.1388 12.61558746140294Epoch: 2026-10-03T23:55Z
TLE epoch observation values (Epoch: 2026-10-03T23:55:36.397Z)
Latitude
-0.00001°
Longitude
131.50102°
Altitude
1,417.347 km
Speed
7.153 km/s
True Right ascension
09h 32m 23s
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
22:12:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,415.915 km
Perigee altitude
1,411.766 km
Semi-major axis
7,791.977 km
Eccentricity
0.00027
Inclination
82.5412°
RAAN
143.0992°
Arg. of periapsis
23.9826°
True anomaly
336.12646°
Mean anomaly
336.1388°
Eccentric anomaly
336.13263°
Mean motion
3.15553 °/min
Orbital period
114.09 mins
BSTAR
-0.000042408
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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. |
|---|---|---|---|---|---|---|---|
| 14 mins | 2026-10-04 04:21:15.653Z | 333.861° NNW | 2026-10-04 04:28:15.653Z | 276.286° WNW | 32.547° | 2026-10-04 04:35:15.653Z | 217.223° SW |
| 14 mins | 2026-10-04 15:15:15.653Z | 158.807° S | 2026-10-04 15:22:15.653Z | 79.55° E | 51.179° | 2026-10-04 15:29:15.653Z | 18.52° NNE |
| 13 mins | 2026-10-04 17:11:15.653Z | 233.893° WSW | 2026-10-04 17:17:15.653Z | 290.376° WNW | 32.737° | 2026-10-04 17:24:15.653Z | 349.585° N |
| 10 mins | 2026-10-05 01:18:15.653Z | 28.141° NE | 2026-10-05 01:22:15.653Z | 60.754° ENE | 20.516° | 2026-10-05 01:28:15.653Z | 108.527° ESE |
| 14 mins | 2026-10-05 03:12:15.653Z | 349.372° N | 2026-10-05 03:19:15.653Z | 223.459° SW | 77.39° | 2026-10-05 03:26:15.653Z | 180.219° SSW |
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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