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 14781U 84021B 24349.17736083 .00002706 00000-0 29873-3 0 9990
2 14781 97.7302 313.4677 0007262 191.0142 169.0917 14.88246205196242
Epoch (UTC): | 14 December 2024 04:15:23 |
Eccentricity: | 0.0007262 |
inclination: | 97.7302° |
perigee height: | 598 km |
apogee height: | 608 km |
right ascension of ascending node: | 313.4677° |
argument of perigee: | 191.0142° |
revolutions per day: | 14.88246205 |
mean anomaly at epoch: | 169.0917° |
orbit number at epoch: | 19624 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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