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DASH/VEP 3, 27368

Orbit data source: Space-Track

DASH/VEP 3, 27368 is a payload satellite owned by NASDA (JP) in HEO that was launched on Mon, 04 Feb 2002 UTC via an H-IIA 2024 launch vehicle from the Tanegashima Space Center (TNSTA). 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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Identifier
27368, 2002-003B
Orbit
HEO
Country
Flag of JPJP / JPN
Related business
Manufacturer
NASDA?
Mission
Civil Technology
Bus & Motor
VEP, Unknown motor
Mass
~330 kg wet, ~330 kg dry
Launch date (UTC)
2002-02-04 (24 years ago)
Launch vehicle
H-IIA 2024
Launch site
Tanegashima Space Center (TNSTA)
Object type
Payload
Rocket body
Debris
Shape & HBR
Hex Cyl, Unknown HBR
Radar Cross Section
0.344 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 DASH/VEP 3
1 27368U 02003B   25348.36883586  .00000218  00000-0  61861-3 0  9996
2 27368  28.9611 317.6219 7143944 197.4130 112.1693  2.36981423201645
Epoch: 2025-12-14T08:51Z
TLE epoch observation values (Epoch: 2025-12-14T08:51:07.418Z)
Latitude
-0.00003°
Longitude
101.54656°
Altitude
30,182.218 km
Speed
2.243 km/s
True Right ascension
21h 10m 26s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
13:22:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,369.341 km
Perigee altitude
410.096 km
Semi-major axis
23,767.855 km
Eccentricity
0.71439
Inclination
28.9611°
RAAN
317.6219°
Arg. of periapsis
197.413°
True anomaly
162.65354°
Mean anomaly
112.1693°
Eccentric anomaly
139.01492°
Mean motion
0.59232 °/min
Orbital period
607.78 mins
BSTAR
0.00061861
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Other satellites on launch #3 in the year 2002 (2002-02-04 UTC)

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