NORAD 67685
GXIBA-1
Time
- Local time
- -
- -
Position
- Latitude
- -
- Longitude
- -
- Altitude
- -
Speed
- Miles per hour
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- Kilometers per second
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- Miles per second
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From your location
- Azimuth
- -
- Elevation
- -
- Right ascension
- -
- Declination
- -
- Local sidereal time
- -
Sunlight
- Day / night
- -
Identity
- NORAD ID
- 67685
- International designator
- 1998-067YC
- Launch date
- Nov 20, 1998
- Launch site
- TYURATAM MISSILE AND SPACE COMPLEX
- Radar size (RCS)
- Medium (0.1–1 m²)
Radio
- Uplink
- -
- Downlink
- 401.140 MHz · MSK AX.100 Mode 5
- Beacon
- -
- Mode
- MSK AX.100 Mode 5
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 DopplerMode U - Transmitter
Transmitter · MSK AX.100 Mode 5
- Downlink
- 401.140 MHz
- CTCSS
- -
- Baud
- 2,400
Recent receptions
SatNOGS Network-
Orbit data
- TLE epoch
- 2026-11-05 04:38:35 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 91 minutes, on an orbit tilted 51.6° from the equator, between 309 and 333 km up. Earth is drawn to scale.
Drag to turn · pinch to zoom · it moves live
About GXIBA-1
GXIBA-1 is a satellite from MEX, launched on Nov 20, 1998 from Tyuratam Missile and Space Complex.
It circles Earth every 91 minutes (15.9 times a day), between 308 and 321 km up, on an orbit tilted 51.6° to the equator, so its path covers latitudes up to 52° 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 26 days its lowest point went from 330 km to 308 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.