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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Identifier
68128, 2026-046B
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Firefly
Mission
Spacecraft
Bus & Motor
FIREFLY A2, Unknown motor
Mass
909 kg wet, 909 kg dry
Launch date (UTC)
2026-03-12 (3 months ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 1.7 m
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 FIREFLY ALPHA R/B
1 68128U 26046B   26170.79394967  .00043875  00000-0  45721-3 0  9992
2 68128 123.0906 296.8318 0009100 148.3469 211.8143 15.64110639 15574
Epoch: 2026-06-19T19:03Z
TLE epoch observation values (Epoch: 2026-06-19T19:03:17.251Z)
Latitude
0.00002°
Longitude
102.99209°
Altitude
382.335 km
Speed
7.679 km/s
True Right ascension
19h 47m 19s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
08:42:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
381.603 km
Perigee altitude
369.311 km
Semi-major axis
6,753.594 km
Eccentricity
0.00091
Inclination
123.0906°
RAAN
296.8318°
Arg. of periapsis
148.3469°
True anomaly
211.75938°
Mean anomaly
211.8143°
Eccentric anomaly
211.78684°
Mean motion
3.91058 °/min
Orbital period
92.06 mins
BSTAR
0.00045721
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Other satellites on launch #46 in the year 2026 (2026-03-12 UTC)

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