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, 1.0 m
Radar Cross Section
0.338 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 FIREFLY-3
1 62710U 25009DF 26262.23009857 .00000927 00000-0 95135-4 0 9999
2 62710 97.6989 338.3944 0002593 189.0696 171.0477 14.92738546 91363Epoch: 2026-09-19T05:31Z
TLE epoch observation values (Epoch: 2026-09-19T05:31:20.516Z)
Latitude
-0.00003°
Longitude
-102.5827°
Altitude
594.231 km
Speed
7.562 km/s
True Right ascension
22h 33m 34s
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
05:44:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
588.222 km
Perigee altitude
584.61 km
Semi-major axis
6,964.553 km
Eccentricity
0.00026
Inclination
97.6989°
RAAN
338.3944°
Arg. of periapsis
189.0696°
True anomaly
171.05232°
Mean anomaly
171.0477°
Eccentric anomaly
171.05001°
Mean motion
3.73425 °/min
Orbital period
96.4 mins
BSTAR
0.000095135
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-09-19 17:21:21.518Z | 37.017° NE | 2026-09-19 17:24:21.518Z | 83.674° E | 27.379° | 2026-09-19 17:28:21.518Z | 155.77° SSE |
| 5 mins | 2026-09-19 18:58:21.518Z | 326.772° NNW | 2026-09-19 19:00:21.518Z | 287.874° WNW | 22.379° | 2026-09-19 19:03:21.518Z | 240.788° WSW |
| 4 mins | 2026-09-20 04:13:21.518Z | 87.165° E | 2026-09-20 04:14:21.518Z | 68.867° E | 18.575° | 2026-09-20 04:17:21.518Z | 22.8° NE |
| 6 mins | 2026-09-20 05:47:21.518Z | 208.323° SW | 2026-09-20 05:49:21.518Z | 251.264° W | 34.366° | 2026-09-20 05:53:21.518Z | 328.196° NNW |
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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