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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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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 AE1D
1 62618U 25009K 25300.96308014 .00038440 00000-0 12115-2 0 9991
2 62618 97.4159 21.1580 0005193 80.1011 280.0817 15.32782649 43589Epoch: 2025-10-27T23:06Z
TLE epoch observation values (Epoch: 2025-10-27T23:06:50.124Z)
Latitude
-0°
Longitude
-2.10824°
Altitude
470.001 km
Speed
7.631 km/s
True Right ascension
01h 24m 37s
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
09:03:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
468.017 km
Perigee altitude
460.91 km
Semi-major axis
6,842.601 km
Eccentricity
0.00052
Inclination
97.4159°
RAAN
21.158°
Arg. of periapsis
80.1011°
True anomaly
280.0231°
Mean anomaly
280.0817°
Eccentric anomaly
280.0524°
Mean motion
3.83452 °/min
Orbital period
93.88 mins
BSTAR
0.0012115
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-28 18:28:28.517Z | 5.845° NNE | 2025-10-28 18:31:28.517Z | 249.524° W | 42.546° | 2025-10-28 18:34:28.517Z | 200.344° SSW |
| 4 mins | 2025-10-29 05:02:28.517Z | 114.836° SE | 2025-10-29 05:03:28.517Z | 85.213° E | 27.823° | 2025-10-29 05:06:28.517Z | 11.429° NNE |
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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