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: 14 hours ago
TLE from 14 hours ago
0 AEPEX
1 68506U 26067CU 26217.45684706 .00004774 00000-0 22645-3 0 9998
2 68506 97.4543 175.2887 0000970 285.5628 74.5500 15.19752429 19308Epoch: 2026-08-05T10:57Z
TLE epoch observation values (Epoch: 2026-08-05T10:57:51.585Z)
Latitude
-0.00003°
Longitude
56.81278°
Altitude
509.499 km
Speed
7.609 km/s
True Right ascension
11h 41m 09s
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
15:22:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.224 km
Perigee altitude
502.889 km
Semi-major axis
6,881.693 km
Eccentricity
0.0001
Inclination
97.4543°
RAAN
175.2887°
Arg. of periapsis
285.5628°
True anomaly
74.56071°
Mean anomaly
74.55°
Eccentric anomaly
74.55536°
Mean motion
3.8019 °/min
Orbital period
94.69 mins
BSTAR
0.00022645
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-08-06 09:39:03.891Z | 31.162° NE | 2026-08-06 09:42:03.891Z | 90.574° ESE | 30.494° | 2026-08-06 09:45:03.891Z | 162.102° S |
| 5 mins | 2026-08-06 21:52:03.891Z | 212.636° SW | 2026-08-06 21:54:03.891Z | 264.044° W | 27.44° | 2026-08-06 21:57:03.891Z | 324.777° NNW |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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