NORAD 60454
EOS-8
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
- 60454
- International designator
- 2024-147A
- Launch date
- Aug 16, 2024
- Launch site
- SIRHARIKOTA
- 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
- 2026-10-26 10:09:42 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 92 minutes, on an orbit tilted 37.4° from the equator, between 1,632,546,387,493 and 1,795,044,412,212 km up. Earth is drawn to scale.
Drag to turn · pinch to zoom · it moves live
About EOS-8
EOS-8 is a satellite from India, launched on Aug 16, 2024 from Sirharikota.
It circles Earth every 92 minutes (15.6 times a day), between 388 and 396 km up, on an orbit tilted 37.4° to the equator, so its path covers latitudes up to 37° north and south.
The map shows where it is right now; the pass list tells you when it next comes over your location.
EOS-08 · Indian Earth observation satellite
- Operated by
- Indian Space Research Organisation
- Built by
- Indian Space Research Organisation
- Mass
- 175 kg
Wikipedia article ↗ · Names and facts: Wikidata (CC0).
Orbit height over the past year
Over the last 15 days its lowest point went from 394 km to 388 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.