FIREFLY ALPHA R/B, 68128
Orbit data source: Space-Track
FIREFLY ALPHA R/B, 68128 is space debris in LEO originally from a launch on Thu, 12 Mar 2026 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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68128 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 FIREFLY ALPHA R/B
1 68128U 26046B 26121.70316958 .00049912 00000-0 60647-3 0 9995
2 68128 123.0904 79.0378 0018921 76.0676 284.2489 15.59914402 7906Epoch: 2026-05-01T16:52Z
TLE epoch observation values (Epoch: 2026-05-01T16:52:33.851Z)
Latitude
0.00001°
Longitude
-33.73487°
Altitude
386.087 km
Speed
7.681 km/s
True Right ascension
05h 16m 09s
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
08:32:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
400.366 km
Perigee altitude
374.763 km
Semi-major axis
6,765.701 km
Eccentricity
0.00189
Inclination
123.0904°
RAAN
79.0378°
Arg. of periapsis
76.0676°
True anomaly
284.03863°
Mean anomaly
284.2489°
Eccentric anomaly
284.14378°
Mean motion
3.90008 °/min
Orbital period
92.31 mins
BSTAR
0.00060647
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Other satellites on launch #46 in the year 2026 (2026-03-12 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-05-02 11:51:17.796Z | 52.535° ENE | 2026-05-02 11:53:17.796Z | 118.23° SE | 43.518° | 2026-05-02 11:55:17.796Z | 219.028° SW |
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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