PELICAN-9 3010, 69019
Orbit data source: Space-Track
PELICAN-9 3010, 69019 is a payload satellite owned by Planet (US) in SSO that was launched on Sun, 03 May 2026 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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69019 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Planet
Mission
Operational spacecraft
Bus & Motor
PELICAN, XE AOCS
Mass
160 kg wet, 146 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 PELICAN-9 3010
1 69019U 26100AR 26175.19275563 -.00000054 00000-0 63393-6 0 9993
2 69019 97.3927 72.8636 0005407 29.8127 330.3416 15.20936520 7876Epoch: 2026-06-24T04:37Z
TLE epoch observation values (Epoch: 2026-06-24T04:37:34.086Z)
Latitude
0°
Longitude
91.11808°
Altitude
502.873 km
Speed
7.615 km/s
True Right ascension
04h 51m 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
07:36:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.697 km
Perigee altitude
496.259 km
Semi-major axis
6,878.115 km
Eccentricity
0.00054
Inclination
97.3927°
RAAN
72.8636°
Arg. of periapsis
29.8127°
True anomaly
330.31092°
Mean anomaly
330.3416°
Eccentric anomaly
330.32626°
Mean motion
3.80486 °/min
Orbital period
94.62 mins
BSTAR
6.3393e-7
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Other satellites on launch #100 in the year 2026 (2026-05-03 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-9 3010 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 | 2026-06-25 06:28:07.851Z | 342.868° N | 2026-06-25 06:30:07.851Z | 270.202° WNW | 34.109° | 2026-06-25 06:33:07.851Z | 214.612° SW |
| 5 mins | 2026-06-25 17:05:07.851Z | 152.163° SSE | 2026-06-25 17:07:07.851Z | 89.371° E | 41.959° | 2026-06-25 17:10:07.851Z | 356.277° N |
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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