NORAD 39678
EGYPTSAT 2
Time
- Local time
- -
- -
Position
- Latitude
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- Longitude
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- Altitude
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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
- 39678
- International designator
- 2014-021A
- Launch date
- Apr 16, 2014
- Launch site
- TYURATAM MISSILE AND SPACE 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
- 2026-11-02 06:03:36 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 99 minutes, on an orbit tilted 51.6° from the equator, between 729 and 740 km up. Earth is drawn to scale.
Drag to turn · pinch to zoom · it moves live
About EGYPTSAT 2
EGYPTSAT 2 is a satellite from EGYP, launched on Apr 16, 2014 from Tyuratam Missile and Space Complex.
It circles Earth every 99 minutes (14.6 times a day), between 705 and 706 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.
EgyptSat 2 · Egyptian space satellite
- Operated by
- National Authority for Remote Sensing and Space Sciences
- Built by
- S.P. Korolev Rocket and Space Corporation Energia
Wikipedia article ↗ · Names and facts: Wikidata (CC0).
Orbit height over the past year
Over the last 22 days its lowest point went from 706 km to 705 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.