TROLL, 62658
Orbit data source: Space-Track
TROLL, 62658 is a Czech payload satellite in SSO that was launched on Tue, 14 Jan 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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62658 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CZ / CZERelated business
Manufacturer
ISIS BV
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.1 m
Radar Cross Section
0.080 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 TROLL
1 62658U 25009BB 25286.16673980 .00016297 00000-0 67128-3 0 9998
2 62658 97.4117 5.0017 0002342 136.3225 223.8198 15.24179683 95748Epoch: 2025-10-13T04:00Z
TLE epoch observation values (Epoch: 2025-10-13T04:00:06.318Z)
Latitude
-0.00004°
Longitude
-76.99803°
Altitude
497.507 km
Speed
7.615 km/s
True Right ascension
00h 20m 00s
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
08:59:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
491.819 km
Perigee altitude
488.602 km
Semi-major axis
6,868.347 km
Eccentricity
0.00023
Inclination
97.4117°
RAAN
5.0017°
Arg. of periapsis
136.3225°
True anomaly
223.80122°
Mean anomaly
223.8198°
Eccentric anomaly
223.81051°
Mean motion
3.81298 °/min
Orbital period
94.41 mins
BSTAR
0.00067128
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Other satellites on launch #9 in the year 2025 (2025-01-14 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.TROLL 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-13 18:44:57.674Z | 344.311° N | 2025-10-13 18:46:57.674Z | 296.553° NW | 29.349° | 2025-10-13 18:49:57.674Z | 224.929° SW |
| 5 mins | 2025-10-14 05:20:57.674Z | 161.252° S | 2025-10-14 05:22:57.674Z | 134.218° SE | 43.122° | 2025-10-14 05:25:57.674Z | 351.829° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
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