FIREFLY ALPHA R/B, 60210
Orbit data source: Space-Track
FIREFLY ALPHA R/B, 60210 is space debris in SSO originally from a launch on Thu, 04 Jul 2024 UTC launched from the Air Force Western Test Range (AFWTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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60210 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 FIREFLY ALPHA R/B
1 60210U 24125H 26088.19266579 .00049637 00000-0 62008-3 0 9990
2 60210 97.2269 310.4793 0026025 119.3682 241.0179 15.59283687 97484Epoch: 2026-03-29T04:37Z
TLE epoch observation values (Epoch: 2026-03-29T04:37:26.324Z)
Latitude
0.00003°
Longitude
54.51753°
Altitude
401.449 km
Speed
7.665 km/s
True Right ascension
20h 41m 55s
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
20:16:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
404.24 km
Perigee altitude
369.03 km
Semi-major axis
6,764.772 km
Eccentricity
0.0026
Inclination
97.2269°
RAAN
310.4793°
Arg. of periapsis
119.3682°
True anomaly
240.75743°
Mean anomaly
241.0179°
Eccentric anomaly
240.88763°
Mean motion
3.90089 °/min
Orbital period
92.29 mins
BSTAR
0.00062008
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Other satellites on launch #125 in the year 2024 (2024-07-04 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.FIREFLY ALPHA R/B Visibility
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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. |
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| FIREFLY ALPHA R/B is likely not visible in the next few days. |
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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