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 30072U 99025PZ 24357.82836023 .00017896 00000-0 69499-2 0 9990
2 30072 99.0743 122.7847 0070458 228.0218 131.4947 14.28552351920853
Epoch (UTC): | 22 December 2024 19:52:50 |
Eccentricity: | 0.0070458 |
inclination: | 99.0743° |
perigee height: | 746 km |
apogee height: | 847 km |
right ascension of ascending node: | 122.7847° |
argument of perigee: | 228.0218° |
revolutions per day: | 14.28552351 |
mean anomaly at epoch: | 131.4947° |
orbit number at epoch: | 92085 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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