HAKUTO-R, 62717
Orbit data source: Space-Track
HAKUTO-R, 62717 is a payload satellite owned by iSpace (JP) in HEO that was launched on Wed, 15 Jan 2025 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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62717 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
JP / JPNRelated business
Manufacturer
ISPACE/ADSL
Mission
Operational Commercial Planetary
Bus & Motor
HAKUTO-R, AOCS
Mass
1,050 kg wet, 340 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 4 Leg, 1.3 m
Radar Cross Section
9.360 m²
Expand to show TLE details & historyLast TLE update: 8 months ago
TLE from 8 months ago
0 HAKUTO-R
1 62717U 25010B 25015.31796730 -.00038243 31373-4 00000-0 0 9992
2 62717 35.1700 0.1839 9650900 345.5700 0.7230 0.10673359 01Epoch: 2025-01-15T07:37Z
TLE epoch observation values (Epoch: 2025-01-15T07:37:52.374Z)
Latitude
25.60567°
Longitude
-93.6906°
Altitude
59,588.328 km
Speed
3.156 km/s
True Right ascension
09h 03m 09s
True Declination
25° 35' 28"
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
11:12:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
362,541.96 km
Perigee altitude
175.762 km
Semi-major axis
187,736.998 km
Eccentricity
0.96509
Inclination
35.17°
RAAN
0.1839°
Arg. of periapsis
345.57°
True anomaly
91.19139°
Mean anomaly
0.723°
Eccentric anomaly
15.49915°
Mean motion
0.02668 °/min
Orbital period
13,492.24 mins
BSTAR
0
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Other satellites on launch #10 in the year 2025 (2025-01-15 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.HAKUTO-R 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. |
|---|---|---|---|---|---|---|---|
| 313 mins | 2025-09-15 18:32:40.040Z | 167.053° S | 2025-09-15 19:08:40.040Z | 179.285° S | 34.211° | 2025-09-15 23:45:40.040Z | 250.267° W |
| 189 mins | 2025-09-16 15:23:40.040Z | 117.86° SE | 2025-09-16 18:32:40.040Z | 160.826° S | 27.584° | 2025-09-16 18:32:40.040Z | 160.826° S |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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