PELICAN-2 3009, 62631
Orbit data source: Space-Track
PELICAN-2 3009, 62631 is a payload satellite owned by Planet (US) in SSO that was launched on Tue, 14 Jan 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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62631 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-2 3009
1 62631U 25009Y 26261.50714486 .00004272 00000-0 10664-3 0 9991
2 62631 97.2027 351.1143 0000728 50.3425 309.7886 15.40714450 93926Epoch: 2026-09-18T12:10Z
TLE epoch observation values (Epoch: 2026-09-18T12:10:17.315Z)
Latitude
-0.00005°
Longitude
171.11312°
Altitude
446.806 km
Speed
7.644 km/s
True Right ascension
23h 24m 27s
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
06:37:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
441.426 km
Perigee altitude
440.433 km
Semi-major axis
6,819.066 km
Eccentricity
0.00007
Inclination
97.2027°
RAAN
351.1143°
Arg. of periapsis
50.3425°
True anomaly
309.78219°
Mean anomaly
309.7886°
Eccentric anomaly
309.78539°
Mean motion
3.85439 °/min
Orbital period
93.4 mins
BSTAR
0.00010664
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Other satellites on launch #9 in the year 2025 (2025-01-14 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-2 3009 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 | 2026-09-19 18:21:19.983Z | 41.138° NE | 2026-09-19 18:23:19.983Z | 81.149° E | 25.49° | 2026-09-19 18:26:19.983Z | 152.448° SSE |
| 4 mins | 2026-09-20 06:24:19.983Z | 197.48° SSW | 2026-09-20 06:25:19.983Z | 232.769° WSW | 49.624° | 2026-09-20 06:28:19.983Z | 335.464° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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