NORAD 58578
QPS-SAR-5 TSUKUYOMI-I
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
- 58578
- International designator
- 2023-196A
- Launch date
- Dec 15, 2023
- Launch site
- Rocket Lab Launch Complex
- 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
- 2026-10-28 13:00:38 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 94 minutes, on an orbit tilted 42.0° from the equator, between 1,101,046 and 1,142,075 km up. Earth is drawn to scale.
Drag to turn · pinch to zoom · it moves live
About QPS-SAR-5 TSUKUYOMI-I
QPS-SAR-5 TSUKUYOMI-I is a satellite from Japan, launched on Dec 15, 2023 from Rocket Lab Launch Complex.
It circles Earth every 94 minutes (15.3 times a day), between 472 and 508 km up, on an orbit tilted 42.0° to the equator, so its path covers latitudes up to 42° 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-5 · 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 17 days its lowest point went from 472 km to 472 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.