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 25509U 98061B 23083.14014983 .00002490 00000-0 47103-3 0 9994
2 25509 31.4324 355.6689 0344189 121.6942 241.7716 14.31074274276383
Epoch (UTC): | 24 March 2023 03:21:48 |
Eccentricity: | 0.0344189 |
inclination: | 31.4324° |
perigee height: | 541 km |
apogee height: | 1035 km |
right ascension of ascending node: | 355.6689° |
argument of perigee: | 121.6942° |
revolutions per day: | 14.31074274 |
mean anomaly at epoch: | 241.7716° |
orbit number at epoch: | 27638 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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