AE1C, 62649
Orbit data source: Space-Track
AE1C, 62649 is a payload satellite owned by ArkEdge (JP) in SSO that was launched on Tue, 14 Jan 2025 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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62649 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
JP / JPNRelated business
Manufacturer
ArkEdge
Mission
Operational Commercial Technology
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 + 2 Pan, 0.3 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 AE1C
1 62649U 25009AS 25300.19201133 .00026526 00000-0 89857-3 0 9994
2 62649 97.4219 20.4002 0002198 67.0914 293.0558 15.30546408 43461Epoch: 2025-10-27T04:36Z
TLE epoch observation values (Epoch: 2025-10-27T04:36:29.778Z)
Latitude
-0.00011°
Longitude
-84.52125°
Altitude
476.695 km
Speed
7.628 km/s
True Right ascension
01h 21m 36s
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
06:34:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
472.639 km
Perigee altitude
469.628 km
Semi-major axis
6,849.27 km
Eccentricity
0.00022
Inclination
97.4219°
RAAN
20.4002°
Arg. of periapsis
67.0914°
True anomaly
293.03262°
Mean anomaly
293.0558°
Eccentric anomaly
293.04421°
Mean motion
3.82892 °/min
Orbital period
94.02 mins
BSTAR
0.00089857
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Other satellites on launch #9 in the year 2025 (2025-01-14 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.AE1C 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-28 18:50:48.138Z | 328.988° NNW | 2025-10-28 18:51:48.138Z | 296.514° NW | 29.75° | 2025-10-28 18:54:48.138Z | 223.282° SW |
| 5 mins | 2025-10-29 05:23:48.138Z | 152.023° SSE | 2025-10-29 05:25:48.138Z | 38.999° NE | 41.624° | 2025-10-29 05:28:48.138Z | 353.778° N |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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