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 28097U 03054C 24307.75100659 0.00000800 00000-0 55824-3 0 05
2 28097 63.4080 265.4691 0564919 3.0530 356.9470 13.41072917 06
Epoch (UTC): | 02 November 2024 18:01:26 |
Eccentricity: | 0.0564919 |
inclination: | 63.4080° |
perigee height: | 682 km |
apogee height: | 1528 km |
right ascension of ascending node: | 265.4691° |
argument of perigee: | 3.0530° |
revolutions per day: | 13.41072917 |
mean anomaly at epoch: | 356.9470° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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