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: 14 hours ago
TLE from 14 hours ago
0 AE1C
1 62649U 25009AS 25353.47590622 .00019310 00000-0 58483-3 0 9991
2 62649 97.4190 73.8073 0001927 180.0930 180.0313 15.34203789 51629Epoch: 2025-12-19T11:25Z
TLE epoch observation values (Epoch: 2025-12-19T11:25:18.297Z)
Latitude
0.00001°
Longitude
174.16454°
Altitude
467.714 km
Speed
7.632 km/s
True Right ascension
04h 55m 13s
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
00:48:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
461.552 km
Perigee altitude
458.916 km
Semi-major axis
6,838.371 km
Eccentricity
0.00019
Inclination
97.419°
RAAN
73.8073°
Arg. of periapsis
180.093°
True anomaly
180.03129°
Mean anomaly
180.0313°
Eccentric anomaly
180.03129°
Mean motion
3.83808 °/min
Orbital period
93.8 mins
BSTAR
0.00058483
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-20 04:47:03.274Z | 117.531° SE | 2025-12-20 04:50:03.274Z | 58.251° ENE | 18.244° | 2025-12-20 04:52:03.274Z | 22.699° NE |
| 4 mins | 2025-12-20 06:21:03.274Z | 231.603° WSW | 2025-12-20 06:22:03.274Z | 253.697° W | 19.213° | 2025-12-20 06:25:03.274Z | 314.517° NW |
| 4 mins | 2025-12-20 17:45:03.274Z | 60.017° ENE | 2025-12-20 17:46:03.274Z | 83.315° E | 21.016° | 2025-12-20 17:49:03.274Z | 148.233° 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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