View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 45U 60007A 25136.51903899 .00000450 00000-0 13802-3 0 9999
2 45 66.6943 329.0630 0242360 88.6564 274.2287 14.35529432379977
Epoch (UTC): | 16 May 2025 12:27:24 |
Eccentricity: | 0.0242360 |
inclination: | 66.6943° |
perigee height: | 600 km |
apogee height: | 946 km |
right ascension of ascending node: | 329.0630° |
argument of perigee: | 88.6564° |
revolutions per day: | 14.35529432 |
mean anomaly at epoch: | 274.2287° |
orbit number at epoch: | 37997 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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