FRONTIERSAT, 69015
Orbit data source: Space-Track
FRONTIERSAT, 69015 is a payload satellite owned by Calgary (CA) in SSO that was launched on Sun, 03 May 2026 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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69015 intel report (Beta)
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Identifier
Orbit
Country
CARelated business
Manufacturer
Calgary
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
~5 kg wet, ~5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.1 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 FRONTIERSAT
1 69015U 26100AM 26220.65315234 .00004417 00000-0 19373-3 0 9993
2 69015 97.3931 117.6555 0006922 206.4017 153.6867 15.22465801 14807Epoch: 2026-08-08T15:40Z
TLE epoch observation values (Epoch: 2026-08-08T15:40:32.362Z)
Latitude
-0.00008°
Longitude
-74.64074°
Altitude
505.768 km
Speed
7.609 km/s
True Right ascension
07h 50m 37s
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
22:28:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.126 km
Perigee altitude
490.61 km
Semi-major axis
6,873.505 km
Eccentricity
0.00069
Inclination
97.3931°
RAAN
117.6555°
Arg. of periapsis
206.4017°
True anomaly
153.72183°
Mean anomaly
153.6867°
Eccentric anomaly
153.70427°
Mean motion
3.80869 °/min
Orbital period
94.52 mins
BSTAR
0.00019373
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Other satellites on launch #100 in the year 2026 (2026-05-03 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.FRONTIERSAT 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 | 2026-08-09 17:02:57.544Z | 152.582° SSE | 2026-08-09 17:05:57.544Z | 41.755° NE | 39.84° | 2026-08-09 17:08:57.544Z | 355.887° N |
| 5 mins | 2026-08-10 06:06:57.544Z | 10.155° NNE | 2026-08-10 06:08:57.544Z | 206.791° SW | 44.057° | 2026-08-10 06:11:57.544Z | 194.343° SSW |
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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