Showing default

OUTPOST MISSION 1, 56226

Orbit data source: Space-Track

OUTPOST MISSION 1, 56226 is a payload satellite owned by Outpost Tech (US) in SSO that was launched on Mon, 12 Jun 2023 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
56226, 2023-084BK
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Outpost Tech
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
3 kg wet, 3 kg dry
Launch date (UTC)
2023-06-12 (3 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 16 hours ago

TLE from 16 hours ago
0 OUTPOST MISSION 1
1 56226U 23084BK  26112.68508692  .00103872  00000-0  55665-3 0  9995
2 56226  97.6024 269.9983 0001416 158.5041 201.6285 15.80006927160204
Epoch: 2026-04-22T16:26Z
TLE epoch observation values (Epoch: 2026-04-22T16:26:31.509Z)
Latitude
-0.00011°
Longitude
172.62406°
Altitude
334.47 km
Speed
7.707 km/s
True Right ascension
17h 59m 59s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
15:27:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
328.266 km
Perigee altitude
326.367 km
Semi-major axis
6,705.453 km
Eccentricity
0.00014
Inclination
97.6024°
RAAN
269.9983°
Arg. of periapsis
158.5041°
True anomaly
201.62252°
Mean anomaly
201.6285°
Eccentric anomaly
201.62551°
Mean motion
3.95276 °/min
Orbital period
91.08 mins
BSTAR
0.00055665
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
|