AE1A, 68487
Orbit data source: Space-Track
AE1A, 68487 is a payload satellite owned by ArkEdge (JP) 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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68487 intel report (Beta)
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Identifier
Orbit
Country
JP / JPNRelated business
Manufacturer
ArkEdge
Mission
Operational spacecraft
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 0.6 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 AE1A
1 68487U 26067BZ 26171.43288532 .00003632 00000-0 35737-3 0 9998
2 68487 97.7543 129.6670 0001052 152.6212 207.5062 14.92710712 12210Epoch: 2026-06-20T10:23Z
TLE epoch observation values (Epoch: 2026-06-20T10:23:21.291Z)
Latitude
-0.00012°
Longitude
65.18072°
Altitude
593.181 km
Speed
7.563 km/s
True Right ascension
08h 38m 40s
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
15:15:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.238 km
Perigee altitude
585.772 km
Semi-major axis
6,964.642 km
Eccentricity
0.00011
Inclination
97.7543°
RAAN
129.667°
Arg. of periapsis
152.6212°
True anomaly
207.50063°
Mean anomaly
207.5062°
Eccentric anomaly
207.50342°
Mean motion
3.73418 °/min
Orbital period
96.41 mins
BSTAR
0.00035737
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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.AE1A 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-22 09:36:52.932Z | 31.034° NE | 2026-06-22 09:39:52.932Z | 80.715° E | 31.009° | 2026-06-22 09:43:52.932Z | 165.597° S |
| 5 mins | 2026-06-22 20:27:52.932Z | 109.006° ESE | 2026-06-22 20:29:52.932Z | 68.972° E | 22.703° | 2026-06-22 20:32:52.932Z | 17.543° NNE |
| 5 mins | 2026-06-22 22:02:52.932Z | 218.43° SW | 2026-06-22 22:04:52.932Z | 254.675° W | 22.647° | 2026-06-22 22:07:52.932Z | 312.602° NW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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