FFLY-1, 65320
Orbit data source: Space-Track
FFLY-1, 65320 is a payload satellite owned by Pixxel (US) in SSO that was launched on Tue, 26 Aug 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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Identifier
Orbit
Country
USRelated 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, 14.5 m
Radar Cross Section
0.338 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 FFLY-1
1 65320U 25188F 26124.19439123 .00001255 00000-0 12643-3 0 9999
2 65320 97.7384 200.1758 0009752 327.2488 32.8126 14.92907497 37347Epoch: 2026-05-04T04:39Z
TLE epoch observation values (Epoch: 2026-05-04T04:39:55.402Z)
Latitude
0.00001°
Longitude
-91.89213°
Altitude
586.21 km
Speed
7.57 km/s
True Right ascension
13h 20m 42s
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
22:49:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
592.683 km
Perigee altitude
579.1 km
Semi-major axis
6,964.029 km
Eccentricity
0.00098
Inclination
97.7384°
RAAN
200.1758°
Arg. of periapsis
327.2488°
True anomaly
32.87322°
Mean anomaly
32.8126°
Eccentric anomaly
32.8429°
Mean motion
3.73467 °/min
Orbital period
96.39 mins
BSTAR
0.00012643
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Other satellites on launch #188 in the year 2025 (2025-08-26 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.FFLY-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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-05-04 18:06:05.097Z | 5.075° NNE | 2026-05-04 18:09:05.097Z | 310.496° NW | 42.349° | 2026-05-04 18:13:05.097Z | 202.995° SW |
| 6 mins | 2026-05-05 04:56:05.097Z | 155.887° SSE | 2026-05-05 04:58:05.097Z | 123.079° SE | 42.045° | 2026-05-05 05:02:05.097Z | 352.828° N |
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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