PELICAN-6 300D, 66703
Orbit data source: Space-Track
PELICAN-6 300D, 66703 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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66703 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: 1 day ago
TLE from 1 day ago
0 PELICAN-6 300D
1 66703U 25276AP 26238.22459828 .00018630 00000-0 57668-3 0 9998
2 66703 97.3590 312.9931 0000938 48.6553 311.4770 15.33518147 41259Epoch: 2026-08-26T05:23Z
TLE epoch observation values (Epoch: 2026-08-26T05:23:25.291Z)
Latitude
-0.00003°
Longitude
-102.34294°
Altitude
468.01 km
Speed
7.632 km/s
True Right ascension
20h 51m 58s
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
03:52:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
462.913 km
Perigee altitude
461.63 km
Semi-major axis
6,840.408 km
Eccentricity
0.00009
Inclination
97.359°
RAAN
312.9931°
Arg. of periapsis
48.6553°
True anomaly
311.46895°
Mean anomaly
311.477°
Eccentric anomaly
311.47297°
Mean motion
3.83637 °/min
Orbital period
93.84 mins
BSTAR
0.00057668
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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-6 300D 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 | 2026-08-27 17:57:31.798Z | 10.78° NNE | 2026-08-27 18:00:31.798Z | 1.431° NNE | 42.881° | 2026-08-27 18:03:31.798Z | 194.739° SSW |
| 4 mins | 2026-08-28 04:31:31.798Z | 115.077° SE | 2026-08-28 04:33:31.798Z | 61.223° ENE | 24.059° | 2026-08-28 04:35:31.798Z | 18.967° 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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