GONETS D1 9, 27060
Orbit data source: Space-Track
GONETS D1 9, 27060 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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27060 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: 9 hours ago
TLE from 9 hours ago
0 GONETS D1 9
1 27060U 01058F 25342.86971884 .00000037 00000-0 14789-3 0 9998
2 27060 82.5398 318.2632 0008953 24.7474 335.4045 12.63057704103801Epoch: 2025-12-08T20:52Z
TLE epoch observation values (Epoch: 2025-12-08T20:52:23.707Z)
Latitude
-0.00006°
Longitude
-72.69814°
Altitude
1,406.739 km
Speed
7.16 km/s
True Right ascension
21h 13m 03s
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
04:01:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,414.641 km
Perigee altitude
1,400.7 km
Semi-major axis
7,785.807 km
Eccentricity
0.0009
Inclination
82.5398°
RAAN
318.2632°
Arg. of periapsis
24.7474°
True anomaly
335.36176°
Mean anomaly
335.4045°
Eccentric anomaly
335.38313°
Mean motion
3.15928 °/min
Orbital period
113.95 mins
BSTAR
0.00014789
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Other satellites on launch #58 in the year 2001 (2001-12-28 UTC)
Did you know?
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 9 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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2025-12-09 08:53:43.901Z | 19.053° NNE | 2025-12-09 08:59:43.901Z | 69.709° E | 22.768° | 2025-12-09 09:05:43.901Z | 118.119° SE |
| 14 mins | 2025-12-09 10:48:43.901Z | 344.842° N | 2025-12-09 10:54:43.901Z | 284.244° WNW | 42.604° | 2025-12-09 11:02:43.901Z | 187.66° SSW |
| 10 mins | 2025-12-09 21:43:43.901Z | 119.76° SE | 2025-12-09 21:47:43.901Z | 84.995° E | 21.836° | 2025-12-09 21:53:43.901Z | 35.425° NE |
| 14 mins | 2025-12-09 23:35:43.901Z | 200.187° SSW | 2025-12-09 23:41:43.901Z | 259.546° W | 42.465° | 2025-12-09 23:49:43.901Z | 1.722° NNE |
| 4 mins | 2025-12-10 01:37:43.901Z | 292.757° NW | 2025-12-10 01:38:43.901Z | 300.203° NW | 11.753° | 2025-12-10 01:41:43.901Z | 322.002° NNW |
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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