Showing default

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.

Loading next visibility...
Identifier
69019, 2026-100AR
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Planet
Mission
Operational Commercial Imaging
Bus & Motor
PELICAN, XE AOCS
Mass
160 kg wet, 146 kg dry
Launch date (UTC)
2026-05-03 (5 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
1.955 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 21 hours ago

TLE from 21 hours ago
0 PELICAN-9 3010
1 69019U 26100AR  26265.71711894  .00020418  00000-0  76039-3 0  9996
2 69019  97.2512 161.3955 0003288 114.9861 245.1721 15.27491307 21660
Epoch: 2026-09-22T17:12Z
TLE epoch observation values (Epoch: 2026-09-22T17:12:39.076Z)
Latitude
0.00004°
Longitude
-98.34591°
Altitude
487.368 km
Speed
7.621 km/s
True Right ascension
10h 45m 34s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
07:32:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
482.519 km
Perigee altitude
478.009 km
Semi-major axis
6,858.401 km
Eccentricity
0.00033
Inclination
97.2512°
RAAN
161.3955°
Arg. of periapsis
114.9861°
True anomaly
245.13791°
Mean anomaly
245.1721°
Eccentric anomaly
245.155°
Mean motion
3.82128 °/min
Orbital period
94.21 mins
BSTAR
0.00076039
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|