NORAD 5485
SHINSEI (MS-F2)
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
- 5485
- International designator
- 1971-080A
- Launch date
- Sep 28, 1971
- Launch site
- KAGOSHIMA SPACE CENTER UNIVERSITY OF TOKYO
- Radar size (RCS)
- Medium (0.1–1 m²)
Radio
- Uplink
- -
- Downlink
- 136.694 MHz · CW
- Beacon
- -
- Mode
- CW
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 Dopplercarrier wave
Transmitter · Space Research · CW
- Downlink
- 136.694 MHz
- CTCSS
- -
- Baud
- -
Recent receptions
SatNOGS Network-
Orbit data
- TLE epoch
- 2026-10-22 08:30:06 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 113 minutes, on an orbit tilted 32.1° from the equator, between 870 and 1,868 km up. Earth is drawn to scale.
Drag to turn · pinch to zoom · it moves live
About SHINSEI (MS-F2)
SHINSEI (MS-F2) is a satellite from Japan, launched on Sep 28, 1971 from Kagoshima Space Center University of Tokyo.
It circles Earth every 113 minutes (12.7 times a day), between 869 and 1,860 km up, on an orbit tilted 32.1° to the equator, so its path covers latitudes up to 32° north and south.
The map shows where it is right now; the pass list tells you when it next comes over your location.
Orbit height over the past year
Over the last 11 days its lowest point went from 869 km to 869 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.