PELICAN-5 300C, 66667
Orbit data source: Space-Track
PELICAN-5 300C, 66667 is a payload satellite owned by Planet (US) in SSO that was launched on Fri, 28 Nov 2025 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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66667 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
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 PELICAN-5 300C
1 66667U 25276B 26092.14815191 .00058397 00000-0 21238-2 0 9992
2 66667 97.4199 167.4133 0002328 245.6367 114.4630 15.28035099 18904Epoch: 2026-04-02T03:33Z
TLE epoch observation values (Epoch: 2026-04-02T03:33:20.325Z)
Latitude
0.00005°
Longitude
-76.42219°
Altitude
485.449 km
Speed
7.622 km/s
True Right ascension
11h 09m 39s
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
08:09:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
480.239 km
Perigee altitude
477.046 km
Semi-major axis
6,856.779 km
Eccentricity
0.00023
Inclination
97.4199°
RAAN
167.4133°
Arg. of periapsis
245.6367°
True anomaly
114.48728°
Mean anomaly
114.463°
Eccentric anomaly
114.47514°
Mean motion
3.82264 °/min
Orbital period
94.18 mins
BSTAR
0.0021238
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Other satellites on launch #276 in the year 2025 (2025-11-28 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-5 300C 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 | 2026-04-03 04:49:45.383Z | 155.71° SSE | 2026-04-03 04:52:45.383Z | 71.969° E | 41.867° | 2026-04-03 04:55:45.383Z | 355.817° N |
| 5 mins | 2026-04-03 17:50:45.383Z | 12.34° NNE | 2026-04-03 17:52:45.383Z | 15.177° NNE | 44.497° | 2026-04-03 17:55:45.383Z | 192.692° 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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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