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ORIGAMISAT-2, 68795

Orbit data source: Space-Track

ORIGAMISAT-2, 68795 is a Japanese payload satellite in SSO that was launched on Thu, 23 Apr 2026 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). 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/68795?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

68795, 2026-088D

Orbit

SSO

Country

JP / JPN

Related business

None

Manufacturer

Unknown

Mission

Operational spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2026-04-23 (2 months ago)

Launch vehicle

ELECTRON

Launch site

Rocket Lab Launch Complex (RLLC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 14.5 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago

0 ORIGAMISAT-2
1 68795U 26088D   26171.34560186  .00010363  00000-0  66061-3 0  9994
2 68795  97.5085 320.6709 0016215  71.4280 288.8709 15.08799773  8775

Epoch: 2026-06-20T08:17Z

TLE epoch observation values (Epoch: 2026-06-20T08:17:40.000Z)

Latitude

0.00001°

Longitude

-72.30732°

Altitude

539.326 km

Speed

7.595 km/s

True Right ascension

21h 22m 41s

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

07:19:45

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

548.064 km

Perigee altitude

525.639 km

Semi-major axis

6,914.989 km

Eccentricity

0.00162

Inclination

97.5085°

RAAN

320.6709°

Arg. of periapsis

71.428°

True anomaly

288.69496°

Mean anomaly

288.8709°

Eccentric anomaly

288.78294°

Mean motion

3.77447 °/min

Orbital period

95.38 mins

BSTAR

0.00066061

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Other satellites on launch #88 in the year 2026 (2026-04-23 UTC)

OBJECT E, 68796

ELECTRON R/B (1), 68800 (Decayed)

ELECTRON R/B (2), 68801 (Decayed)

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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.

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ORIGAMISAT-2 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	2026-06-20 23:12:00.140Z	347.88° N	2026-06-20 23:14:00.140Z	276.643° WNW	37.074°	2026-06-20 23:17:00.140Z	213.099° SW
6 mins	2026-06-21 09:54:00.140Z	157.405° SSE	2026-06-21 09:56:00.140Z	123.319° SE	42.26°	2026-06-21 10:00:00.140Z	352.379° N

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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 ORIGAMISAT-2, 68795 on other resources

View ORIGAMISAT-2, 68795 on NASA - NSSDCA Website

View ORIGAMISAT-2, 68795 on Heavens-Above

View ORIGAMISAT-2, 68795 on Keep Track

View ORIGAMISAT-2, 68795 on Celestrak

View ORIGAMISAT-2, 68795 on Gunter's Space Page

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

ORIGAMISAT-2, 68795

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 12 hours ago

TLE from 12 hours ago

TLE epoch observation values (Epoch: 2026-06-20T08:17:40.000Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #88 in the year 2026 (2026-04-23 UTC)

ORIGAMISAT-2 Visibility forecast

Co-orbital & Co-planar RSOs

Check out ORIGAMISAT-2, 68795 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 12 hours ago