HOKUSHIN1, 69648
Orbit data source: Space-Track
HOKUSHIN1, 69648 is a payload satellite owned by Tohoku (CIS) in LEO that was delivered to the ISS. 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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69648 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
Tohoku
Mission
Operational spacecraft
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4 kg wet, 4 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
BOX, 0.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 HOKUSHIN1
1 69648U 98067YH 26249.40749871 .00017150 00000-0 27262-3 0 9992
2 69648 51.6308 256.6869 0005704 133.0023 227.1446 15.53408612 12260Epoch: 2026-09-06T09:46Z
TLE epoch observation values (Epoch: 2026-09-06T09:46:47.888Z)
Latitude
-0.00003°
Longitude
124.48429°
Altitude
410.157 km
Speed
7.665 km/s
True Right ascension
17h 06m 44s
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
13:36:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
411.163 km
Perigee altitude
403.422 km
Semi-major axis
6,785.43 km
Eccentricity
0.00057
Inclination
51.6308°
RAAN
256.6869°
Arg. of periapsis
133.0023°
True anomaly
227.09671°
Mean anomaly
227.1446°
Eccentric anomaly
227.12065°
Mean motion
3.88309 °/min
Orbital period
92.71 mins
BSTAR
0.00027262
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Other satellites on launch #67 in the year 1998 (1998-11-20 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.HOKUSHIN1 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 | 2026-09-07 02:56:28.074Z | 198.798° SSW | 2026-09-07 02:58:28.074Z | 142.2° SSE | 38.533° | 2026-09-07 03:01:28.074Z | 67.68° E |
| 4 mins | 2026-09-07 04:33:28.074Z | 287.698° WNW | 2026-09-07 04:35:28.074Z | 343.38° N | 26.043° | 2026-09-07 04:37:28.074Z | 27.692° NE |
| 5 mins | 2026-09-07 09:25:28.074Z | 326.332° NNW | 2026-09-07 09:27:28.074Z | 39.432° NE | 46.619° | 2026-09-07 09:30:28.074Z | 108.315° ESE |
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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