FIREFLY-3, 62710
Orbit data source: Space-Track
FIREFLY-3, 62710 is a payload satellite owned by Pixxel (IN) in SSO that was launched on Tue, 14 Jan 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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62710 intel report (Beta)
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Identifier
Orbit
Country
IN / INDRelated business
Manufacturer
Pixxel
Mission
Operational Commercial Imaging
Bus & Motor
FIREFLY, Unknown motor
Mass
60 kg wet, 60 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.7 m
Radar Cross Section
0.338 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 FIREFLY-3
1 62710U 25009DF 26171.46881475 .00000706 00000-0 73750-4 0 9991
2 62710 97.7060 249.5638 0004475 129.8151 230.3463 14.92740754 77829Epoch: 2026-06-20T11:15Z
TLE epoch observation values (Epoch: 2026-06-20T11:15:05.594Z)
Latitude
-0.00001°
Longitude
172.1075°
Altitude
594.43 km
Speed
7.562 km/s
True Right ascension
16h 38m 15s
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
07:23:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
589.526 km
Perigee altitude
583.293 km
Semi-major axis
6,964.546 km
Eccentricity
0.00045
Inclination
97.706°
RAAN
249.5638°
Arg. of periapsis
129.8151°
True anomaly
230.30683°
Mean anomaly
230.3463°
Eccentric anomaly
230.32657°
Mean motion
3.73425 °/min
Orbital period
96.4 mins
BSTAR
0.00007375
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Other satellites on launch #9 in the year 2025 (2025-01-14 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-3 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-21 05:03:44.256Z | 157.845° S | 2026-06-21 05:07:44.256Z | 82.504° E | 42.842° | 2026-06-21 05:11:44.256Z | 353.371° N |
| 6 mins | 2026-06-21 18:23:44.256Z | 357.527° N | 2026-06-21 18:26:44.256Z | 256.695° W | 38.721° | 2026-06-21 18:29:44.256Z | 209.136° SW |
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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