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 30634U 99025ANR 24357.90921455 .00011686 00000-0 66905-2 0 9997
2 30634 99.2720 324.8543 0130333 2.2076 56.9436 14.05426603907501
Epoch (UTC): | 22 December 2024 21:49:16 |
Eccentricity: | 0.0130333 |
inclination: | 99.2720° |
perigee height: | 780 km |
apogee height: | 969 km |
right ascension of ascending node: | 324.8543° |
argument of perigee: | 2.2076° |
revolutions per day: | 14.05426603 |
mean anomaly at epoch: | 56.9436° |
orbit number at epoch: | 90750 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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