NORAD 59447
QPS-SAR-7 TSUKUYOMI-II
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
- 59447
- International designator
- 2024-066F
- Launch date
- Apr 7, 2024
- Launch site
- AIR FORCE EASTERN TEST RANGE
- 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
- 2026-10-27 23:31:10 UTC
- TLE age
- -
Radio data from SatNOGS DB and SatNOGS Network, licensed CC BY-SA 4.0.
About QPS-SAR-7 TSUKUYOMI-II
QPS-SAR-7 TSUKUYOMI-II is a satellite from Japan, launched on Apr 7, 2024 from Air Force Eastern Test Range.
It circles Earth every 95 minutes (15.1 times a day), between 534 and 536 km up, on an orbit tilted 45.6° to the equator, so its path covers latitudes up to 46° north and south.
The map shows where it is right now; the pass list tells you when it next comes over your location.
QPS-SAR-7 · Japanese commercial synthetic aperture radar satellite
- Operated by
- iQPS
- Built by
- iQPS
- Mass
- 100 kg
Names and facts: Wikidata (CC0).
Orbit height over the past year
Over the last 16 days its lowest point went from 534 km to 534 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.