EDDA-1 300E, 69017
Orbit data source: Space-Track
EDDA-1 300E, 69017 is a payload satellite owned by Planet (US) in SSO that was launched on Sun, 03 May 2026 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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69017 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Planet
Mission
Operational Commercial Imaging
Bus & Motor
PELICAN, XE AOCS
Mass
160 kg wet, 146 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
1.955 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 EDDA-1 300E
1 69017U 26100AP 26317.83335647 .00005538 00000-0 17814-3 0 9995
2 69017 97.3299 213.2863 0012670 78.6977 242.5453 15.32575378 1304Epoch: 2026-11-13T20:00Z
TLE epoch observation values (Epoch: 2026-11-13T20:00:01.999Z)
Latitude
-38.78477°
Longitude
-133.76858°
Altitude
487.02 km
Speed
7.618 km/s
True Right ascension
14h 36m 44s
True Declination
-38° 36' 37"
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
21:09:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
473.748 km
Perigee altitude
456.407 km
Semi-major axis
6,843.215 km
Eccentricity
0.00127
Inclination
97.3299°
RAAN
213.2863°
Arg. of periapsis
78.6977°
True anomaly
242.41656°
Mean anomaly
242.5453°
Eccentric anomaly
242.48092°
Mean motion
3.83401 °/min
Orbital period
93.9 mins
BSTAR
0.00017814
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Other satellites on launch #100 in the year 2026 (2026-05-03 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.EDDA-1 300E 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 | 2026-11-14 06:07:17.930Z | 8.981° NNE | 2026-11-14 06:10:17.930Z | 345.445° N | 65.792° | 2026-11-14 06:13:17.930Z | 197.999° SSW |
| 4 mins | 2026-11-14 16:42:17.930Z | 105.676° ESE | 2026-11-14 16:43:17.930Z | 75.142° E | 29.216° | 2026-11-14 16:46:17.930Z | 11.606° NNE |
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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