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, 0.2 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 FRONTIERSAT
1 69015U 26100AM 26264.94413376 .00005733 00000-0 24648-3 0 9992
2 69015 97.3862 161.2230 0009834 68.4985 291.7299 15.22999254 21546Epoch: 2026-09-21T22:39Z
TLE epoch observation values (Epoch: 2026-09-21T22:39:33.156Z)
Latitude
-0.00008°
Longitude
-179.48184°
Altitude
497.397 km
Speed
7.617 km/s
True Right ascension
10h 44m 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
07:32:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.519 km
Perigee altitude
487.003 km
Semi-major axis
6,871.898 km
Eccentricity
0.00098
Inclination
97.3862°
RAAN
161.223°
Arg. of periapsis
68.4985°
True anomaly
291.62517°
Mean anomaly
291.7299°
Eccentric anomaly
291.67754°
Mean motion
3.81003 °/min
Orbital period
94.49 mins
BSTAR
0.00024648
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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 | 2026-09-23 17:21:22.417Z | 174.628° S | 2026-09-23 17:24:22.417Z | 242.072° WSW | 70.99° | 2026-09-23 17:27:22.417Z | 342.303° N |
| 6 mins | 2026-09-24 06:24:22.417Z | 356.571° N | 2026-09-24 06:27:22.417Z | 281.389° WNW | 46.317° | 2026-09-24 06:30:22.417Z | 213.949° SW |
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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