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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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Identifier
62658, 2025-009BB
Orbit
SSO
Country
Flag of CZCZ / CZE
Related business
Manufacturer
ISIS BV
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
2025-01-14 (1 year ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.1 m
Radar Cross Section
0.080 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 21 hours ago

TLE from 21 hours ago
0 TROLL
1 62658U 25009BB  26080.20697567  .00011353  00000-0  41280-3 0  9992
2 62658  97.3920 162.6099 0000951  44.1293 316.0022 15.28421770120004
Epoch: 2026-03-21T04:58Z
TLE epoch observation values (Epoch: 2026-03-21T04:58:02.697Z)
Latitude
-0.0001°
Longitude
-90.63233°
Altitude
483.163 km
Speed
7.624 km/s
True Right ascension
10h 50m 26s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
07:02:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
478.136 km
Perigee altitude
476.832 km
Semi-major axis
6,855.621 km
Eccentricity
0.0001
Inclination
97.392°
RAAN
162.6099°
Arg. of periapsis
44.1293°
True anomaly
315.99463°
Mean anomaly
316.0022°
Eccentric anomaly
315.99841°
Mean motion
3.8236 °/min
Orbital period
94.15 mins
BSTAR
0.0004128
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Documentation

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