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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.

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Iframe URL

https://www.satcat.com/sats-embedded/56226?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

56226, 2023-084BK

Orbit

SSO

Country

US

Related business

Outpost Technologies (US)

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: 13 hours ago

TLE from 13 hours ago

0 OUTPOST MISSION 1
1 56226U 23084BK  26064.38169159  .00102711  00000-0  87944-3 0  9995
2 56226  97.5958 217.1991 0004583 265.7363  94.3375 15.69104078152604

Epoch: 2026-03-05T09:09Z

TLE epoch observation values (Epoch: 2026-03-05T09:09:38.153Z)

Latitude

0.00004°

Longitude

-83.34273°

Altitude

364.847 km

Speed

7.69 km/s

True Right ascension

14h 28m 47s

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

02:33:45

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

361.458 km

Perigee altitude

355.283 km

Semi-major axis

6,736.507 km

Eccentricity

0.00046

Inclination

97.5958°

RAAN

217.1991°

Arg. of periapsis

265.7363°

True anomaly

94.38986°

Mean anomaly

94.3375°

Eccentric anomaly

94.36368°

Mean motion

3.92546 °/min

Orbital period

91.71 mins

BSTAR

0.00087944

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Other satellites on launch #84 in the year 2023 (2023-06-12 UTC)

SKYKRAFT-3D, 57956

OBJECT BQ, 56231 (Decayed)

ISTANBUL, 56230 (Decayed)

SKYKRAFT-3, 56229 (Decayed)

SKYKRAFT-3B, 56227 (Decayed)

SKYKRAFT-3C, 56228 (Decayed)

OBJECT CA, 60449 (Decayed)

FOSSASAT2E15 (FEROX), 56938 (Decayed)

FOSSASAT2E17 (FEROX), 56935 (Decayed)

EIVE, 56937 (Decayed)

GEISAT PRECURSOR, 56934

SPACEBEE-179, 56969 (Decayed)

TOMORROW-R2, 56962

SPEI SATELLES, 56991 (Decayed)

Did you know?

You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.

Click here to try in Sandbox

OUTPOST MISSION 1 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	2026-03-05 23:29:28.926Z	341.141° N	2026-03-05 23:31:28.926Z	281.921° WNW	24.877°	2026-03-05 23:33:28.926Z	229.99° WSW

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Co-orbital & Co-planar RSOs

Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions

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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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Check out OUTPOST MISSION 1, 56226 on other resources

View OUTPOST MISSION 1, 56226 on NASA - NSSDCA Website

View OUTPOST MISSION 1, 56226 on Heavens-Above

View OUTPOST MISSION 1, 56226 on Keep Track

View OUTPOST MISSION 1, 56226 on Celestrak

View OUTPOST MISSION 1, 56226 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

Documentation

Go to standalone docs website

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