PELICAN-5, 66667
Orbit data source: Space-Track
PELICAN-5, 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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Edit Public Description
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: 21 hours ago
TLE from 21 hours ago
0 PELICAN-5
1 66667U 25276B 26034.21582814 .00004887 00000-0 24377-3 0 9992
2 66667 97.4355 110.0798 0004545 91.9942 268.1813 15.17972369 10082Epoch: 2026-02-03T05:10Z
TLE epoch observation values (Epoch: 2026-02-03T05:10:47.551Z)
Latitude
0.00004°
Longitude
-101.01829°
Altitude
515.157 km
Speed
7.606 km/s
True Right ascension
07h 20m 19s
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
04:10:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
512.069 km
Perigee altitude
505.809 km
Semi-major axis
6,887.076 km
Eccentricity
0.00045
Inclination
97.4355°
RAAN
110.0798°
Arg. of periapsis
91.9942°
True anomaly
268.12925°
Mean anomaly
268.1813°
Eccentric anomaly
268.15527°
Mean motion
3.79744 °/min
Orbital period
94.8 mins
BSTAR
0.00024377
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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 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 | 2026-02-04 05:02:14.916Z | 170.381° S | 2026-02-04 05:05:14.916Z | 272.489° WNW | 44.721° | 2026-02-04 05:08:14.916Z | 345.676° N |
| 5 mins | 2026-02-04 18:08:14.916Z | 354.087° N | 2026-02-04 18:10:14.916Z | 305.514° NW | 36.734° | 2026-02-04 18:13:14.916Z | 214.34° SW |
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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