Showing default

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.

Loading next visibility...
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: 2 days ago

TLE from 2 days ago
0 DASH/VEP 3
1 27368U 02003B   26148.19063157  .00000204  00000-0  11069-2 0  9999
2 27368  28.6400 256.4672 7125755 295.9663   9.2512  2.37113728205552
Epoch: 2026-05-28T04:34Z
TLE epoch observation values (Epoch: 2026-05-28T04:34:30.567Z)
Latitude
0.00005°
Longitude
-57.97529°
Altitude
2,528.631 km
Speed
8.528 km/s
True Right ascension
17h 05m 33s
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
04:41:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,310.989 km
Perigee altitude
450.789 km
Semi-major axis
23,759.026 km
Eccentricity
0.71258
Inclination
28.64°
RAAN
256.4672°
Arg. of periapsis
295.9663°
True anomaly
64.74767°
Mean anomaly
9.2512°
Eccentric anomaly
29.11879°
Mean motion
0.59265 °/min
Orbital period
607.44 mins
BSTAR
0.0011069
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #3 in the year 2002 (2002-02-04 UTC)

Documentation

Showing up to 5 results
|