EDISON-1, 62610
Orbit data source: Space-Track
EDISON-1, 62610 is a Danish payload satellite 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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62610 intel report (Beta)
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Identifier
Orbit
Country
DK / DENRelated business
Manufacturer
Space Inventor
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 8U, Unknown motor
Mass
~15 kg wet, ~15 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 0.3 m
Radar Cross Section
0.180 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 EDISON-1
1 62610U 25009B 26171.19387432 .00010954 00000-0 36057-3 0 9998
2 62610 97.4000 253.7027 0003940 301.2627 58.8228 15.31667459 79411Epoch: 2026-06-20T04:39Z
TLE epoch observation values (Epoch: 2026-06-20T04:39:10.741Z)
Latitude
-0.00003°
Longitude
-84.50405°
Altitude
472.547 km
Speed
7.63 km/s
True Right ascension
16h 54m 48s
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
07:24:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
470.484 km
Perigee altitude
465.09 km
Semi-major axis
6,845.924 km
Eccentricity
0.00039
Inclination
97.4°
RAAN
253.7027°
Arg. of periapsis
301.2627°
True anomaly
58.86144°
Mean anomaly
58.8228°
Eccentric anomaly
58.84212°
Mean motion
3.83173 °/min
Orbital period
93.95 mins
BSTAR
0.00036057
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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.EDISON-1 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 | 2026-06-21 05:52:18.103Z | 189.944° SSW | 2026-06-21 05:54:18.103Z | 235.35° WSW | 35.537° | 2026-06-21 05:57:18.103Z | 332.152° NNW |
| 5 mins | 2026-06-21 18:51:18.103Z | 341.384° N | 2026-06-21 18:53:18.103Z | 278.868° WNW | 30.871° | 2026-06-21 18:56:18.103Z | 218.896° SW |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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