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 days ago
TLE from 4 days ago
0 GONETS D1 8
1 27059U 01058E 26155.26137983 -.00000014 00000-0 -13565-3 0 9995
2 27059 82.5417 221.0210 0000731 282.5710 77.5299 12.61556741124943Epoch: 2026-06-04T06:16Z
TLE epoch observation values (Epoch: 2026-06-04T06:16:23.217Z)
Latitude
0.00001°
Longitude
-125.78392°
Altitude
1,419.13 km
Speed
7.151 km/s
True Right ascension
14h 44m 05s
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
17:41:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,414.418 km
Perigee altitude
1,413.279 km
Semi-major axis
7,791.986 km
Eccentricity
0.00007
Inclination
82.5417°
RAAN
221.021°
Arg. of periapsis
282.571°
True anomaly
77.53808°
Mean anomaly
77.5299°
Eccentric anomaly
77.53399°
Mean motion
3.15552 °/min
Orbital period
114.09 mins
BSTAR
-0.00013565
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-08 13:42:17.256Z | 40.101° NE | 2026-06-08 13:45:17.256Z | 62.478° ENE | 12.684° | 2026-06-08 13:48:17.256Z | 84.177° E |
| 15 mins | 2026-06-08 15:34:17.256Z | 357.595° N | 2026-06-08 15:41:17.256Z | 65.165° ENE | 43.344° | 2026-06-08 15:49:17.256Z | 164.024° S |
| 10 mins | 2026-06-08 17:31:17.256Z | 317.5° NNW | 2026-06-08 17:36:17.256Z | 274.484° WNW | 20.797° | 2026-06-08 17:41:17.256Z | 235.36° WSW |
| 15 mins | 2026-06-09 04:22:17.256Z | 174.757° S | 2026-06-09 04:29:17.256Z | 107.649° ESE | 43.543° | 2026-06-09 04:37:17.256Z | 12.168° NNE |
| 11 mins | 2026-06-09 06:20:17.256Z | 250.194° W | 2026-06-09 06:25:17.256Z | 292.148° WNW | 21.481° | 2026-06-09 06:31:17.256Z | 340.923° 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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