FALCONSAT-6, 43815
Orbit data source: Space-Track
FALCONSAT-6, 43815 is a payload satellite owned by USAF SMC (US) in SSO that was launched on Mon, 03 Dec 2018 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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43815 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
USAF Academy
Mission
Operational Defense Technology
Bus & Motor
FALCONSAT, Unknown motor
Mass
181 kg wet, 181 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Ant, 2.0 m
Radar Cross Section
0.551 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 FALCONSAT-6
1 43815U 18099BK 25259.15079457 .00004078 00000-0 17052-3 0 9996
2 43815 97.4110 333.1519 0017166 185.6650 204.4514 15.24031100371943Epoch: 2025-09-16T03:37Z
TLE epoch observation values (Epoch: 2025-09-16T03:37:08.65Z)
Latitude
29.81157°
Longitude
-80.7299°
Altitude
508.305 km
Speed
7.607 km/s
True Right ascension
21h 55m 36s
True Declination
29° 39' 29"
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
05:37:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.448 km
Perigee altitude
478.866 km
Semi-major axis
6,868.794 km
Eccentricity
0.00172
Inclination
97.411°
RAAN
333.1519°
Arg. of periapsis
185.665°
True anomaly
204.37014°
Mean anomaly
204.4514°
Eccentric anomaly
204.41075°
Mean motion
3.81261 °/min
Orbital period
94.42 mins
BSTAR
0.00017052
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Other satellites on launch #99 in the year 2018 (2018-12-03 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.FALCONSAT-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 | 2025-09-16 18:14:05.922Z | 354.404° N | 2025-09-16 18:17:05.922Z | 260.06° W | 34.347° | 2025-09-16 18:19:05.922Z | 217.397° SW |
| 5 mins | 2025-09-17 04:51:05.922Z | 142.709° SSE | 2025-09-17 04:53:05.922Z | 49.654° ENE | 39.176° | 2025-09-17 04:56:05.922Z | 357.322° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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