AE1D, 62618
Orbit data source: Space-Track
AE1D, 62618 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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62618 intel report (Beta)
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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 AE1D
1 62618U 25009K 26150.20535469 .00119093 00000-0 15813-2 0 9990
2 62618 97.3965 239.3090 0001250 13.7142 346.4147 15.57816511 76648Epoch: 2026-05-30T04:55Z
TLE epoch observation values (Epoch: 2026-05-30T04:55:42.645Z)
Latitude
-0.00004°
Longitude
-82.34341°
Altitude
396.296 km
Speed
7.673 km/s
True Right ascension
15h 57m 14s
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
21:29:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
391.739 km
Perigee altitude
390.047 km
Semi-major axis
6,769.03 km
Eccentricity
0.00013
Inclination
97.3965°
RAAN
239.309°
Arg. of periapsis
13.7142°
True anomaly
346.41133°
Mean anomaly
346.4147°
Eccentric anomaly
346.41302°
Mean motion
3.89721 °/min
Orbital period
92.37 mins
BSTAR
0.0015813
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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.AE1D 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 | 2026-05-31 18:29:09.053Z | 32.131° NE | 2026-05-31 18:31:09.053Z | 82.802° E | 31.686° | 2026-05-31 18:34:09.053Z | 169.568° S |
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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