NORAD 28937
HIMAWARI 7
Time
- Local time
- -
- -
Position
- Latitude
- -
- Longitude
- -
- Altitude
- -
Speed
- Miles per hour
- -
- Kilometers per second
- -
- Miles per second
- -
From your location
- Azimuth
- -
- Elevation
- -
- Right ascension
- -
- Declination
- -
- Local sidereal time
- -
Sunlight
- Day / night
- -
Identity
- NORAD ID
- 28937
- International designator
- 2006-004A
- Launch date
- Feb 18, 2006
- Launch site
- TANEGASHIMA SPACE CENTER
- Radar size (RCS)
- Large (over 1 m²)
Radio
- Uplink
- -
- Downlink
- -
- Beacon
- -
- Mode
- -
Active transmitters from SatNOGS DB, licensed CC BY-SA 4.0.
Your station
- Grid locator
- -
Live
- Azimuth
- -
- Elevation
- -
- Range
- -
- Range rate
- -
- Naked-eye visibility
- -
- Sub-satellite grid
- -
- Footprint diameter
- -
Upcoming passes
Next 48 h · your local timeUse your location to predict passes.
Mutual visibility
With another station · next 48 hUse your location to find mutual windows.
Transmitters
Nominal · add location for Doppler-
Recent receptions
SatNOGS Network-
Orbit data
- TLE epoch
- 2026-11-04 21:43:06 UTC
- TLE age
- -
Radio data from SatNOGS DB and SatNOGS Network, licensed CC BY-SA 4.0.
Its orbit in 3D
Goes round Earth once every 24.2 hours, on an orbit tilted 6.1° from the equator, between 36,083 and 36,182 km up. Earth is drawn to scale.
Drag to turn · pinch to zoom · it moves live
About HIMAWARI 7
HIMAWARI 7 is a satellite from Japan, launched on Feb 18, 2006 from Tanegashima Space Center.
It sits in geostationary orbit about 35,800 km above the equator near 58°E, turning with Earth so it stays over the same spot.
The map shows where it is right now; the pass list tells you when it next comes over your location.
MTSat-2 · decommissioned Japanese geostationary navigation satellite
- Operated by
- Japan Civil Aviation Bureau, Japan Meteorological Agency
- Built by
- Boeing Defense, Space & Security, Mitsubishi Electric
- Mass
- 4,650 kg
Names and facts: Wikidata (CC0).
Orbit height over the past year
Over the last 365 days its lowest point went from 36,076 km to 36,076 km. Sudden rises are engine burns that lift the orbit; slow declines are drag from the thin upper atmosphere.
From Space-Track element sets, one point a day.