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: 9 hours ago
TLE from 9 hours ago
0 FIREFLY-1
1 62701U 25009CW 26093.55585851 .00003422 00000-0 33593-3 0 9991
2 62701 97.7085 173.2235 0003530 185.8947 174.2231 14.92836160 66181Epoch: 2026-04-03T13:20Z
TLE epoch observation values (Epoch: 2026-04-03T13:20:26.175Z)
Latitude
-0.00007°
Longitude
141.22615°
Altitude
594.589 km
Speed
7.561 km/s
True Right ascension
11h 32m 53s
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
03:55:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
588.571 km
Perigee altitude
583.654 km
Semi-major axis
6,964.249 km
Eccentricity
0.00035
Inclination
97.7085°
RAAN
173.2235°
Arg. of periapsis
185.8947°
True anomaly
174.22717°
Mean anomaly
174.2231°
Eccentric anomaly
174.22514°
Mean motion
3.73449 °/min
Orbital period
96.4 mins
BSTAR
0.00033593
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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 | 2026-04-04 05:33:50.496Z | 188.024° SSW | 2026-04-04 05:35:50.496Z | 232.634° WSW | 38.883° | 2026-04-04 05:39:50.496Z | 337.466° NNW |
| 4 mins | 2026-04-04 17:17:50.496Z | 68.963° E | 2026-04-04 17:18:50.496Z | 88.84° E | 20.114° | 2026-04-04 17:21:50.496Z | 141.047° SSE |
| 5 mins | 2026-04-04 18:52:50.496Z | 329.54° NNW | 2026-04-04 18:54:50.496Z | 283.201° WNW | 25.18° | 2026-04-04 18:57:50.496Z | 232.885° WSW |
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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