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: 12 hours ago
TLE from 12 hours ago
0 PELICAN-5 300C
1 66667U 25276B 26141.18379183 .00008435 00000-0 30380-3 0 9994
2 66667 97.4166 216.2558 0005537 92.1223 268.0651 15.28809762 26390Epoch: 2026-05-21T04:24Z
TLE epoch observation values (Epoch: 2026-05-21T04:24:39.614Z)
Latitude
0°
Longitude
-88.7419°
Altitude
482.602 km
Speed
7.624 km/s
True Right ascension
14h 25m 01s
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
01:45:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
480.119 km
Perigee altitude
472.528 km
Semi-major axis
6,854.461 km
Eccentricity
0.00055
Inclination
97.4166°
RAAN
216.2558°
Arg. of periapsis
92.1223°
True anomaly
268.00169°
Mean anomaly
268.0651°
Eccentric anomaly
268.03339°
Mean motion
3.82458 °/min
Orbital period
94.13 mins
BSTAR
0.0003038
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-05-21 17:32:54.363Z | 30.403° NE | 2026-05-21 17:34:54.363Z | 74.007° E | 34.194° | 2026-05-21 17:37:54.363Z | 168.928° S |
| 4 mins | 2026-05-22 05:40:54.363Z | 216.248° SW | 2026-05-22 05:42:54.363Z | 264.153° W | 23.948° | 2026-05-22 05:44:54.363Z | 311.306° NW |
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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