EDDA-1 300F, 69018
Orbit data source: Space-Track
EDDA-1 300F, 69018 is an American payload satellite 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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69018 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
None
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: 18 hours ago
TLE from 18 hours ago
0 EDDA-1 300F
1 69018U 26100AQ 26220.68112507 .00001764 00000-0 73059-4 0 9991
2 69018 97.3596 117.6867 0003053 89.0308 271.1279 15.25217628 14812Epoch: 2026-08-08T16:20Z
TLE epoch observation values (Epoch: 2026-08-08T16:20:49.206Z)
Latitude
-0.00008°
Longitude
-84.7073°
Altitude
493.19 km
Speed
7.618 km/s
True Right ascension
07h 50m 44s
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
00:37:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
489.185 km
Perigee altitude
484.993 km
Semi-major axis
6,865.226 km
Eccentricity
0.00031
Inclination
97.3596°
RAAN
117.6867°
Arg. of periapsis
89.0308°
True anomaly
271.09292°
Mean anomaly
271.1279°
Eccentric anomaly
271.11041°
Mean motion
3.81558 °/min
Orbital period
94.35 mins
BSTAR
0.000073059
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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 300F 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 | 2026-08-09 17:40:41.622Z | 202.63° SW | 2026-08-09 17:42:41.622Z | 260.803° W | 32.34° | 2026-08-09 17:45:41.622Z | 329.748° NNW |
| 4 mins | 2026-08-10 06:42:41.622Z | 329.984° NNW | 2026-08-10 06:44:41.622Z | 275.798° WNW | 24.557° | 2026-08-10 06:46:41.622Z | 235.248° WSW |
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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