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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Edit Public Description
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: 17 hours ago
TLE from 17 hours ago
0 GONETS D1 8
1 27059U 01058E 25256.32813918 .00000035 00000-0 13746-3 0 9994
2 27059 82.5435 30.0396 0002740 141.3009 218.8278 12.61548190 91669Epoch: 2025-09-13T07:52Z
TLE epoch observation values (Epoch: 2025-09-13T07:52:31.225Z)
Latitude
-0.00003°
Longitude
-80.65359°
Altitude
1,420.953 km
Speed
7.15 km/s
True Right ascension
02h 00m 09s
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
17:25:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,416.019 km
Perigee altitude
1,411.749 km
Semi-major axis
7,792.021 km
Eccentricity
0.00027
Inclination
82.5435°
RAAN
30.0396°
Arg. of periapsis
141.3009°
True anomaly
218.80812°
Mean anomaly
218.8278°
Eccentric anomaly
218.81796°
Mean motion
3.1555 °/min
Orbital period
114.09 mins
BSTAR
0.00013746
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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 | 2025-09-14 08:43:13.493Z | 148.666° SSE | 2025-09-14 08:50:13.493Z | 80.287° E | 32.494° | 2025-09-14 08:57:13.493Z | 22.459° NNE |
| 14 mins | 2025-09-14 10:38:13.493Z | 220.95° SW | 2025-09-14 10:45:13.493Z | 293.335° NW | 33.692° | 2025-09-14 10:52:13.493Z | 353.865° N |
| 7 mins | 2025-09-14 18:47:13.493Z | 38.914° NE | 2025-09-14 18:50:13.493Z | 62.473° ENE | 14.883° | 2025-09-14 18:54:13.493Z | 92.524° ESE |
| 15 mins | 2025-09-14 20:39:13.493Z | 354.845° N | 2025-09-14 20:46:13.493Z | 49.309° ENE | 44.495° | 2025-09-14 20:54:13.493Z | 169.658° S |
| 8 mins | 2025-09-14 22:37:13.493Z | 308.94° NW | 2025-09-14 22:40:13.493Z | 284.097° WNW | 18.071° | 2025-09-14 22:45:13.493Z | 244.319° 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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