FIREFLY-1, 62701
Orbit data source: Space-Track
FIREFLY-1, 62701 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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62701 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, 0.9 m
Radar Cross Section
0.338 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 FIREFLY-1
1 62701U 25009CW 26215.95444840 .00001210 00000-0 12240-3 0 9992
2 62701 97.7047 293.0892 0004269 154.8727 205.2701 14.92785625 84446Epoch: 2026-08-03T22:54Z
TLE epoch observation values (Epoch: 2026-08-03T22:54:24.341Z)
Latitude
-0.00003°
Longitude
-3.04236°
Altitude
594.99 km
Speed
7.561 km/s
True Right ascension
19h 32m 21s
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
21:01:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
589.243 km
Perigee altitude
583.296 km
Semi-major axis
6,964.407 km
Eccentricity
0.00043
Inclination
97.7047°
RAAN
293.0892°
Arg. of periapsis
154.8727°
True anomaly
205.24923°
Mean anomaly
205.2701°
Eccentric anomaly
205.25966°
Mean motion
3.73437 °/min
Orbital period
96.4 mins
BSTAR
0.0001224
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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-1 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-08-05 17:18:50.538Z | 43.339° NE | 2026-08-05 17:21:50.538Z | 96.293° ESE | 22.884° | 2026-08-05 17:24:50.538Z | 148.361° SSE |
| 4 mins | 2026-08-05 18:55:50.538Z | 320.863° NNW | 2026-08-05 18:56:50.538Z | 299.892° NW | 22.288° | 2026-08-05 18:59:50.538Z | 243.155° WSW |
| 5 mins | 2026-08-06 05:44:50.538Z | 210.392° SW | 2026-08-06 05:46:50.538Z | 266.593° W | 31.991° | 2026-08-06 05:49:50.538Z | 326.723° NNW |
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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