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 26170.77332706 .00000023 00000-0 25488-5 0 9992
2 62631 97.2641 261.5843 0000781 166.9534 193.1733 15.40721230 79950Epoch: 2026-06-19T18:33Z
TLE epoch observation values (Epoch: 2026-06-19T18:33:35.457Z)
Latitude
-0.00006°
Longitude
75.18908°
Altitude
447.621 km
Speed
7.643 km/s
True Right ascension
17h 26m 20s
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
07:23:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
441.444 km
Perigee altitude
440.379 km
Semi-major axis
6,819.049 km
Eccentricity
0.00008
Inclination
97.2641°
RAAN
261.5843°
Arg. of periapsis
166.9534°
True anomaly
193.17126°
Mean anomaly
193.1733°
Eccentric anomaly
193.17228°
Mean motion
3.85441 °/min
Orbital period
93.4 mins
BSTAR
0.0000025488
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-21 06:33:09.560Z | 206.394° SW | 2026-06-21 06:35:09.560Z | 275.742° WNW | 30.741° | 2026-06-21 06:37:09.560Z | 324.639° NNW |
| 4 mins | 2026-06-21 19:27:09.560Z | 334.626° NNW | 2026-06-21 19:29:09.560Z | 269.676° W | 27.107° | 2026-06-21 19:31:09.560Z | 227.2° WSW |
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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