GEN-3 FM-6, 100682
Orbit data source: Space-Track
GEN-3 FM-6, 100682 is a payload satellite owned by BlackSky Global (US) in LEO that was launched on Fri, 11 Sep 2026 UTC launched from the Rocket Lab Launch Complex (RLLC). 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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100682 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
LeoStella
Mission
Operational spacecraft
Bus & Motor
BSKY, Unknown motor
Mass
138 kg wet, 134 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
BOX+2 PAN, 1.5 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 GEN-3 FM-6
1 A0682U 26208A 26259.47663575 .00005310 00000-0 22855-3 0 9995
2 A0682 36.0163 278.4728 0010540 315.7222 44.2667 15.22168595 819Epoch: 2026-09-16T11:26Z
TLE epoch observation values (Epoch: 2026-09-16T11:26:21.328Z)
Latitude
-0.00001°
Longitude
111.45624°
Altitude
493.129 km
Speed
7.623 km/s
True Right ascension
18h 33m 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
02:01:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.641 km
Perigee altitude
495.136 km
Semi-major axis
6,880.526 km
Eccentricity
0.00105
Inclination
36.0163°
RAAN
278.4728°
Arg. of periapsis
315.7222°
True anomaly
44.35108°
Mean anomaly
44.2667°
Eccentric anomaly
44.30888°
Mean motion
3.80286 °/min
Orbital period
94.67 mins
BSTAR
0.00022855
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Other satellites on launch #207 in the year 2026 (2026-09-11 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.GEN-3 FM-6 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-17 09:57:30.473Z | 244.959° WSW | 2026-09-17 09:59:30.473Z | 210.382° SW | 19.903° | 2026-09-17 10:02:30.473Z | 157.26° SSE |
| 4 mins | 2026-09-18 04:37:30.473Z | 181.675° SSW | 2026-09-18 04:38:30.473Z | 159.368° S | 21.799° | 2026-09-18 04:41:30.473Z | 107.562° ESE |
| 6 mins | 2026-09-18 06:15:30.473Z | 237.656° WSW | 2026-09-18 06:17:30.473Z | 193.98° SSW | 41.76° | 2026-09-18 06:21:30.473Z | 101.609° ESE |
| 5 mins | 2026-09-18 07:55:30.473Z | 246.43° WSW | 2026-09-18 07:57:30.473Z | 188.602° SSW | 41.35° | 2026-09-18 08:00:30.473Z | 121.953° SE |
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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