NORAD 68798
MAGNARO-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
- 68798
- International designator
- 2026-088G
- Launch date
- Apr 23, 2026
- Launch site
- Rocket Lab Launch Complex
- Radar size (RCS)
- Medium (0.1–1 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
- 2026-10-21 09:20:41 UTC
- TLE age
- -
Radio data from SatNOGS DB and SatNOGS Network, licensed CC BY-SA 4.0.
About MAGNARO-II
MAGNARO-II is a satellite from Japan, launched on Apr 23, 2026 from Rocket Lab Launch Complex.
It circles Earth every 95 minutes (15.1 times a day), between 524 and 551 km up, on an orbit tilted 97.5° to the equator, so its path covers latitudes up to 82° north and south.
The map shows where it is right now; the pass list tells you when it next comes over your location.
MAGNARO-II Tigris · Japanese technology demonstration CubeSat
- Operated by
- Nagoya University
- Built by
- Nagoya University
Names and facts: Wikidata (CC0).
Orbit height over the past year
Over the last 10 days its lowest point went from 524 km to 524 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.