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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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Firefly
Mission
Spacecraft
Bus & Motor
FIREFLY A2, Unknown motor
Mass
909 kg wet, 909 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 2.9 m
Radar Cross Section
9.508 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 FIREFLY ALPHA R/B
1 60210U 24125H 25302.55351434 .00031153 00000-0 57953-3 0 9990
2 60210 97.2464 158.3698 0031013 321.5256 38.3783 15.48280747 74093Epoch: 2025-10-29T13:17Z
TLE epoch observation values (Epoch: 2025-10-29T13:17:03.638Z)
Latitude
-0.0001°
Longitude
-79.02034°
Altitude
408.378 km
Speed
7.675 km/s
True Right ascension
10h 33m 28s
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
17:00:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
439.756 km
Perigee altitude
397.598 km
Semi-major axis
6,796.814 km
Eccentricity
0.0031
Inclination
97.2464°
RAAN
158.3698°
Arg. of periapsis
321.5256°
True anomaly
38.59961°
Mean anomaly
38.3783°
Eccentric anomaly
38.48889°
Mean motion
3.87334 °/min
Orbital period
92.94 mins
BSTAR
0.00057953
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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 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 | 2025-10-30 03:47:42.238Z | 352.904° N | 2025-10-30 03:50:42.238Z | 276.331° WNW | 31.012° | 2025-10-30 03:52:42.238Z | 224.67° SW |
| 4 mins | 2025-10-30 14:15:42.238Z | 119.953° SE | 2025-10-30 14:16:42.238Z | 74.605° E | 33.561° | 2025-10-30 14:19:42.238Z | 2.93° NNE |
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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