Showing default

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.

Loading next visibility...
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: 8 hours ago

TLE from 8 hours ago
0 MDS 1
1 27367U 02003A   26149.45946639  .00010145  00000-0  69528-3 0  9992
2 27367  28.5079 285.7403 4141291 323.1377  14.5012  7.17238185391519
Epoch: 2026-05-29T11:01Z
TLE epoch observation values (Epoch: 2026-05-29T11:01:37.896Z)
Latitude
-0.00001°
Longitude
-126.65716°
Altitude
690.68 km
Speed
8.814 km/s
True Right ascension
19h 02m 57s
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
04:41:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
9,688.008 km
Perigee altitude
278.035 km
Semi-major axis
11,361.158 km
Eccentricity
0.41413
Inclination
28.5079°
RAAN
285.7403°
Arg. of periapsis
323.1377°
True anomaly
36.90767°
Mean anomaly
14.5012°
Eccentric anomaly
24.24466°
Mean motion
1.79229 °/min
Orbital period
200.86 mins
BSTAR
0.00069528
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
|