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MDS 1, 27367

Orbit data source: Space-Track

MDS 1, 27367 is a payload satellite owned by NASDA (JP) 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
27367, 2002-003A
Orbit
Active
Country
Flag of JPJP / JPN
Related business
Manufacturer
NEC Toshiba/Kamoi
Mission
Non-operational Civil Technology
Bus & Motor
MDS, AOCS
Mass
449 kg wet, ~440 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
Box + 2 Pan, 1.6 m
Radar Cross Section
5.220 m², Large (>1 m²)

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

TLE from 1 day ago
0 MDS 1
1 27367U 02003A   25260.56468872  .00012375  00000-0  80398-3 0  9990
2 27367  28.5123 352.1237 4200994 348.9137   4.1384  7.07035344373404
Epoch: 2025-09-17T13:33Z
TLE epoch observation values (Epoch: 2025-09-17T13:33:09.105Z)
Latitude
-0.00003°
Longitude
152.09688°
Altitude
308.139 km
Speed
9.191 km/s
True Right ascension
23h 28m 29s
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
07:19:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
9,910.631 km
Perigee altitude
273.416 km
Semi-major axis
11,470.16 km
Eccentricity
0.4201
Inclination
28.5123°
RAAN
352.1237°
Arg. of periapsis
348.9137°
True anomaly
11.12614°
Mean anomaly
4.1384°
Eccentric anomaly
7.12311°
Mean motion
1.76681 °/min
Orbital period
203.76 mins
BSTAR
0.00080398
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Other satellites on launch #3 in the year 2002 (2002-02-04 UTC)

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