Showing default

SOHLA-1 (MAIDO-1), 33496

Orbit data source: Space-Track

SOHLA-1 (MAIDO-1), 33496 is a Japanese payload satellite in SSO that was launched on Fri, 23 Jan 2009 UTC via an H-IIA 202 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
33496, 2009-002E
Orbit
SSO
Country
Flag of JPJP / JPN
Related business
Manufacturer
SOHLA
Mission
Non-operational Amateur Science
Bus & Motor
SOHLA, Unknown motor
Mass
50 kg wet, 50 kg dry
Launch date (UTC)
2009-01-23 (17 years ago)
Launch vehicle
H-IIA 202
Launch site
Tanegashima Space Center (TNSTA)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.3 m
Radar Cross Section
0.375 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago
0 SOHLA-1 (MAIDO-1)
1 33496U 09002E   26103.23239819  .00000305  00000-0  53130-4 0  9999
2 33496  98.1443   7.5879 0004976 212.1516 147.9390 14.74962668924412
Epoch: 2026-04-13T05:34Z
TLE epoch observation values (Epoch: 2026-04-13T05:34:39.203Z)
Latitude
0.00001°
Longitude
82.4986°
Altitude
651.24 km
Speed
7.53 km/s
True Right ascension
00h 30m 21s
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
20:23:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
645.822 km
Perigee altitude
638.835 km
Semi-major axis
7,020.465 km
Eccentricity
0.0005
Inclination
98.1443°
RAAN
7.5879°
Arg. of periapsis
212.1516°
True anomaly
147.96925°
Mean anomaly
147.939°
Eccentric anomaly
147.95413°
Mean motion
3.68973 °/min
Orbital period
97.57 mins
BSTAR
0.00005313
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...

Documentation

Showing up to 5 results
|