PELICAN-7 300E, 69017
Orbit data source: Space-Track
PELICAN-7 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: 14 hours ago
TLE from 14 hours ago
0 PELICAN-7 300E
1 69017U 26100AP 26237.75630605 .00003069 00000-0 12805-3 0 9991
2 69017 97.3674 134.5327 0001178 97.6650 262.4721 15.24416310 17409Epoch: 2026-08-25T18:09Z
TLE epoch observation values (Epoch: 2026-08-25T18:09:04.842Z)
Latitude
-0.00008°
Longitude
-111.75655°
Altitude
495.742 km
Speed
7.617 km/s
True Right ascension
08h 58m 07s
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
23:17:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
490.306 km
Perigee altitude
488.688 km
Semi-major axis
6,867.634 km
Eccentricity
0.00012
Inclination
97.3674°
RAAN
134.5327°
Arg. of periapsis
97.665°
True anomaly
262.45872°
Mean anomaly
262.4721°
Eccentric anomaly
262.46541°
Mean motion
3.81358 °/min
Orbital period
94.4 mins
BSTAR
0.00012805
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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-7 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-08-26 16:21:41.027Z | 107.154° ESE | 2026-08-26 16:23:41.027Z | 69.989° E | 17.103° | 2026-08-26 16:25:41.027Z | 31.924° NE |
| 4 mins | 2026-08-26 17:55:41.027Z | 226.576° WSW | 2026-08-26 17:56:41.027Z | 250.221° W | 22.909° | 2026-08-26 17:59:41.027Z | 316.706° NNW |
| 4 mins | 2026-08-27 05:23:41.027Z | 53.372° ENE | 2026-08-27 05:25:41.027Z | 99.44° ESE | 22.214° | 2026-08-27 05:27:41.027Z | 142.133° SSE |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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