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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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
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 FIREFLY ALPHA R/B
1 68128U 26046B 26102.14767163 .00027471 00000-0 35662-3 0 9995
2 68128 123.0916 352.6331 0018281 43.5958 316.6544 15.58497426 4853Epoch: 2026-04-12T03:32Z
TLE epoch observation values (Epoch: 2026-04-12T03:32:38.828Z)
Latitude
-0.00008°
Longitude
99.11457°
Altitude
384.325 km
Speed
7.685 km/s
True Right ascension
23h 30m 31s
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
19:33:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
404.041 km
Perigee altitude
379.289 km
Semi-major axis
6,769.802 km
Eccentricity
0.00183
Inclination
123.0916°
RAAN
352.6331°
Arg. of periapsis
43.5958°
True anomaly
316.51037°
Mean anomaly
316.6544°
Eccentric anomaly
316.58241°
Mean motion
3.89654 °/min
Orbital period
92.39 mins
BSTAR
0.00035662
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-04-12 14:30:36.989Z | 106.012° ESE | 2026-04-12 14:32:36.989Z | 63.598° ENE | 29.546° | 2026-04-12 14:35:36.989Z | 329.291° NNW |
| 5 mins | 2026-04-13 07:45:36.989Z | 40.414° NE | 2026-04-13 07:47:36.989Z | 9.212° NNE | 39.677° | 2026-04-13 07:50:36.989Z | 236.819° WSW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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