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 spacecraft
Bus & Motor
PELICAN, XE AOCS
Mass
160 kg wet, 146 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 PELICAN-7 300E
1 69017U 26100AP 26174.64645911 .00002708 00000-0 12109-3 0 9991
2 69017 97.4045 72.4193 0001153 80.7400 279.3967 15.22157977 7791Epoch: 2026-06-23T15:30Z
TLE epoch observation values (Epoch: 2026-06-23T15:30:54.067Z)
Latitude
0.00003°
Longitude
-72.12102°
Altitude
502.297 km
Speed
7.613 km/s
True Right ascension
04h 49m 40s
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
05:59:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
497.088 km
Perigee altitude
495.503 km
Semi-major axis
6,874.433 km
Eccentricity
0.00012
Inclination
97.4045°
RAAN
72.4193°
Arg. of periapsis
80.74°
True anomaly
279.38366°
Mean anomaly
279.3967°
Eccentric anomaly
279.39018°
Mean motion
3.80792 °/min
Orbital period
94.54 mins
BSTAR
0.00012109
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-25 05:56:02.693Z | 16.989° NNE | 2026-06-25 06:00:02.693Z | 149.885° SSE | 40.966° | 2026-06-25 06:03:02.693Z | 185.128° SSW |
| 4 mins | 2026-06-25 16:35:02.693Z | 108.292° ESE | 2026-06-25 16:37:02.693Z | 57.892° ENE | 22.563° | 2026-06-25 16:39:02.693Z | 20.039° NNE |
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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