PELICAN-8 300F, 69018
Orbit data source: Space-Track
PELICAN-8 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: 19 hours ago
TLE from 19 hours ago
0 PELICAN-8 300F
1 69018U 26100AQ 26265.71767522 .00009312 00000-0 34982-3 0 9995
2 69018 97.3105 161.9046 0003796 95.4887 264.6785 15.27390071 21684Epoch: 2026-09-22T17:13Z
TLE epoch observation values (Epoch: 2026-09-22T17:13:27.139Z)
Latitude
-0.00004°
Longitude
-98.03761°
Altitude
486.964 km
Speed
7.622 km/s
True Right ascension
10h 47m 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
05:22:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
483.173 km
Perigee altitude
477.966 km
Semi-major axis
6,858.707 km
Eccentricity
0.00038
Inclination
97.3105°
RAAN
161.9046°
Arg. of periapsis
95.4887°
True anomaly
264.63519°
Mean anomaly
264.6785°
Eccentric anomaly
264.65685°
Mean motion
3.82102 °/min
Orbital period
94.22 mins
BSTAR
0.00034982
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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.PELICAN-8 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-23 16:56:38.817Z | 145.946° SSE | 2026-09-23 16:59:38.817Z | 50.692° ENE | 46.764° | 2026-09-23 17:02:38.817Z | 359.641° N |
| 5 mins | 2026-09-24 05:57:38.817Z | 18.915° NNE | 2026-09-24 05:59:38.817Z | 64.961° ENE | 69.664° | 2026-09-24 06:02:38.817Z | 185.355° SSW |
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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