NORAD 68416
PEAKSAT
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
- 68416
- International designator
- 2026-067A
- Launch date
- Mar 30, 2026
- Launch site
- AIR FORCE WESTERN TEST RANGE
- Radar size (RCS)
- Medium (0.1–1 m²)
Radio
- Uplink
- -
- Downlink
- 400.500 MHz · CW400.500 MHz · GFSK Pkst
- Beacon
- -
- Mode
- CW, GFSK Pkst
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 - CW (interval 5min) (20 wpm, Time Unit = 60 ms, Dot = 60 ms , Dash = 180 ms, Element Gap = 60ms , Gap btw Chars = 180 ms)
Transmitter · CW
- Downlink
- 400.500 MHz
- CTCSS
- -
- Baud
- 20
UHF Telemetry | BFSK | Mod Index 1 | Data Rate 50 kbps
Transmitter · GFSK Pkst
- Downlink
- 400.500 MHz
- CTCSS
- -
- Baud
- 50,000
Recent receptions
SatNOGS NetworkLoading…
Orbit data
- TLE epoch
- 2026-10-21 19:15:17 UTC
- TLE age
- -
Radio data from SatNOGS DB and SatNOGS Network, licensed CC BY-SA 4.0.
About PEAKSAT
PEAKSAT is a satellite from GREC, launched on Mar 30, 2026 from Air Force Western Test Range.
It circles Earth every 95 minutes (15.2 times a day), between 501 and 505 km up, on an orbit tilted 97.5° to the equator, so its path covers latitudes up to 83° 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 11 days its lowest point went from 503 km to 501 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.