GONETS D1 7, 27058
Orbit data source: Space-Track
GONETS D1 7, 27058 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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27058 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: 23 hours ago
TLE from 23 hours ago
0 GONETS D1 7
1 27058U 01058D 25256.08088639 .00000031 00000-0 11230-3 0 9992
2 27058 82.5385 19.6164 0002100 255.1620 104.9238 12.62078095 92037Epoch: 2025-09-13T01:56Z
TLE epoch observation values (Epoch: 2025-09-13T01:56:28.584Z)
Latitude
-0.00003°
Longitude
-1.82208°
Altitude
1,417.529 km
Speed
7.152 km/s
True Right ascension
01h 18m 27s
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
17:30:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,413.337 km
Perigee altitude
1,410.065 km
Semi-major axis
7,789.838 km
Eccentricity
0.00021
Inclination
82.5385°
RAAN
19.6164°
Arg. of periapsis
255.162°
True anomaly
104.94705°
Mean anomaly
104.9238°
Eccentric anomaly
104.93543°
Mean motion
3.15682 °/min
Orbital period
114.04 mins
BSTAR
0.0001123
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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 7 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. |
|---|---|---|---|---|---|---|---|
| 16 mins | 2025-09-14 08:27:36.529Z | 167.877° S | 2025-09-14 08:35:36.529Z | 90.388° ESE | 40.848° | 2025-09-14 08:43:36.529Z | 15.088° NNE |
| 12 mins | 2025-09-14 10:25:36.529Z | 241.444° WSW | 2025-09-14 10:30:36.529Z | 285.27° WNW | 25.237° | 2025-09-14 10:37:36.529Z | 345.634° N |
| 11 mins | 2025-09-14 18:31:36.529Z | 24.813° NE | 2025-09-14 18:36:36.529Z | 68.393° E | 22.018° | 2025-09-14 18:42:36.529Z | 116.422° SE |
| 14 mins | 2025-09-14 20:25:36.529Z | 346.078° N | 2025-09-14 20:32:36.529Z | 249.252° W | 43.135° | 2025-09-14 20:39:36.529Z | 186.314° 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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