TROOP-F2, 60557
Orbit data source: Space-Track
TROOP-F2, 60557 is a payload satellite owned by NearSpaceLaunch (US) in SSO that was launched on Fri, 16 Aug 2024 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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60557 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
NearSpaceLaunch
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 + 4 Pan, 0.3 m
Radar Cross Section
0.139 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 TROOP-F2
1 60557U 24149CT 25289.88923106 .00076254 00000-0 15826-2 0 9994
2 60557 97.3923 10.8528 0002957 33.1557 326.9877 15.45423442 65174Epoch: 2025-10-16T21:20Z
TLE epoch observation values (Epoch: 2025-10-16T21:20:29.563Z)
Latitude
-0.00001°
Longitude
25.08714°
Altitude
431.571 km
Speed
7.654 km/s
True Right ascension
00h 43m 24s
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
23:17:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
429.078 km
Perigee altitude
425.053 km
Semi-major axis
6,805.203 km
Eccentricity
0.0003
Inclination
97.3923°
RAAN
10.8528°
Arg. of periapsis
33.1557°
True anomaly
326.96923°
Mean anomaly
326.9877°
Eccentric anomaly
326.97847°
Mean motion
3.86618 °/min
Orbital period
93.12 mins
BSTAR
0.0015826
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Other satellites on launch #149 in the year 2024 (2024-08-16 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.TROOP-F2 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-17 05:14:23.045Z | 146.805° SSE | 2025-10-17 05:17:23.045Z | 70.228° E | 34.798° | 2025-10-17 05:20:23.045Z | 1.545° NNE |
| 4 mins | 2025-10-17 18:07:23.045Z | 39.537° NE | 2025-10-17 18:08:23.045Z | 70.988° E | 34.255° | 2025-10-17 18:11:23.045Z | 171.661° S |
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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