PELICAN-3 300A, 65315
Orbit data source: Space-Track
PELICAN-3 300A, 65315 is a payload satellite owned by Planet (US) in SSO that was launched on Tue, 26 Aug 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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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-3 300A
1 65315U 25188A 26170.77456122 .00000532 00000-0 14988-4 0 9998
2 65315 97.1980 246.8856 0001705 91.8248 268.3194 15.40724259 45719Epoch: 2026-06-19T18:35Z
TLE epoch observation values (Epoch: 2026-06-19T18:35:22.089Z)
Latitude
-0.00004°
Longitude
60.04486°
Altitude
447.129 km
Speed
7.644 km/s
True Right ascension
16h 27m 32s
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
07:24:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
442.063 km
Perigee altitude
439.737 km
Semi-major axis
6,819.037 km
Eccentricity
0.00017
Inclination
97.198°
RAAN
246.8856°
Arg. of periapsis
91.8248°
True anomaly
268.29987°
Mean anomaly
268.3194°
Eccentric anomaly
268.30964°
Mean motion
3.85442 °/min
Orbital period
93.4 mins
BSTAR
0.000014988
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Other satellites on launch #188 in the year 2025 (2025-08-26 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-3 300A 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 | 2026-06-21 05:00:21.011Z | 158.553° S | 2026-06-21 05:03:21.011Z | 85.641° E | 42.536° | 2026-06-21 05:06:21.011Z | 354.797° N |
| 5 mins | 2026-06-21 17:55:21.011Z | 15.344° NNE | 2026-06-21 17:57:21.011Z | 98.784° ESE | 44.7° | 2026-06-21 18:00:21.011Z | 189.544° 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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