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 30060U 99025PM 24358.19824459 .00002352 00000-0 29518-2 0 9997
2 30060 99.3317 244.6501 0348371 234.9018 259.5905 13.42487090874943
Epoch (UTC): | 23 December 2024 04:45:28 |
Eccentricity: | 0.0348371 |
inclination: | 99.3317° |
perigee height: | 839 km |
apogee height: | 1360 km |
right ascension of ascending node: | 244.6501° |
argument of perigee: | 234.9018° |
revolutions per day: | 13.42487090 |
mean anomaly at epoch: | 259.5905° |
orbit number at epoch: | 87494 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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