OUTPOST MISSION 1, 56226 (Decayed)
Orbit data source: Space-Track
OUTPOST MISSION 1, 56226 was a payload satellite owned by Outpost Tech (US) in LEO 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.
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56226 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Outpost Tech
Mission
Decayed Commercial Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
3 kg wet, 3 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 OUTPOST MISSION 1
1 56226U 23084BK 26180.13618669 .14309285 27340-5 11766-3 0 9992
2 56226 97.5783 345.9560 0014201 259.1711 100.7996 16.51722429170951Epoch: 2026-06-29T03:16Z
TLE epoch observation values (Epoch: 2026-06-29T03:16:06.530Z)
Latitude
0.00002°
Longitude
19.70282°
Altitude
139.811 km
Speed
7.821 km/s
True Right ascension
23h 03m 49s
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
05:18:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
140.849 km
Perigee altitude
122.36 km
Semi-major axis
6,509.741 km
Eccentricity
0.00142
Inclination
97.5783°
RAAN
345.956°
Arg. of periapsis
259.1711°
True anomaly
100.9594°
Mean anomaly
100.7996°
Eccentric anomaly
100.8795°
Mean motion
4.13235 °/min
Orbital period
87.12 mins
BSTAR
0.00011766
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Other satellites on launch #84 in the year 2023 (2023-06-12 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.OUTPOST MISSION 1 Visibility
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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. |
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| This satellite is decayed. |
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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