AEPEX, 68506
Orbit data source: Space-Track
AEPEX, 68506 is a payload satellite owned by Colorado (US) in SSO that was launched on Mon, 30 Mar 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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68506 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Colorado
Mission
Operational Amateur Science
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 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 AEPEX
1 68506U 26067CU 26258.33904149 .00006396 00000-0 29821-3 0 9991
2 68506 97.4608 215.7028 0004635 113.7038 246.4684 15.20208218 25513Epoch: 2026-09-15T08:08Z
TLE epoch observation values (Epoch: 2026-09-15T08:08:13.184Z)
Latitude
-0.00002°
Longitude
99.34146°
Altitude
509.576 km
Speed
7.608 km/s
True Right ascension
14h 22m 48s
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
06:20:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
505.369 km
Perigee altitude
498.991 km
Semi-major axis
6,880.317 km
Eccentricity
0.00046
Inclination
97.4608°
RAAN
215.7028°
Arg. of periapsis
113.7038°
True anomaly
246.41971°
Mean anomaly
246.4684°
Eccentric anomaly
246.44406°
Mean motion
3.80304 °/min
Orbital period
94.66 mins
BSTAR
0.00029821
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Other satellites on launch #67 in the year 2026 (2026-03-30 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.AEPEX 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 21:53:07.805Z | 213.956° SW | 2026-09-17 21:55:07.805Z | 266.032° W | 30.879° | 2026-09-17 21:58:07.805Z | 324.982° NNW |
| 4 mins | 2026-09-18 09:24:07.805Z | 67.011° ENE | 2026-09-18 09:25:07.805Z | 89.838° E | 22.126° | 2026-09-18 09:28:07.805Z | 146.723° SSE |
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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