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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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https://www.satcat.com/sats-embedded/62717?theme=dark&initialShowStats=false

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Identifier

62717, 2025-010B

Orbit

HEO

Last TLE update

3 months ago

Origin

iSpace Inc. (JP / JPN)

Manufacturer

ISPACE/ADSL

Mission

Operational Commercial Planetary

Bus & Motor

HAKUTO-R, AOCS

Mass

1,050 kg wet, 340 kg dry

Launch date (UTC)

2025-01-15 (3 months ago)

Launch vehicle

FALCON 9

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box + 4 Leg, 2.6 m

Radar Cross Section

9.360 m²

Expand to show TLE details & history

TLE from 3 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    01

Epoch: 2025-01-15T07:37Z

Definitive object data (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

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

3.77871°

Longitude

-57.18459°

Altitude

349,839.132 km

Speed

0.339 km/s

Apparent Right ascension

11h 32m 11s

Apparent Declination

3° 08' 15"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

06:41:07

Azimuth

98.812° ESE

Elevation

15.189°

Doppler factor

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

BSTAR

Unknown

Orbital period

13492.24 mins

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Other satellites on launch #10 in the year 2025 (2025-01-15 UTC)

BLUE GHOST, 62716 (Decayed)

FALCON 9 DEB, 62718

FALCON 9 R/B, 62719

HAKUTO-R Visibility forecast

Observer location: undefined°, undefined°

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.
601 mins	2025-04-16 00:04:01.474Z	98.814° ESE	2025-04-16 04:53:01.474Z	179.984° S	38.566°	2025-04-16 10:05:01.474Z	264.373° W
12 mins	2025-04-16 23:52:01.474Z	97.386° ESE	2025-04-17 00:04:01.474Z	99.392° ESE	12.399°	2025-04-17 00:04:01.474Z	99.392° ESE

Authenticating...

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Check out HAKUTO-R, 62717 on other resources

View HAKUTO-R, 62717 on NASA - NSSDCA Website

View HAKUTO-R, 62717 on Heavens-Above

View HAKUTO-R, 62717 on Keep Track

View HAKUTO-R, 62717 on Celestrak

View HAKUTO-R, 62717 on Gunter's Space Page

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