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 30129U 99025SJ 24279.98065053 .00004128 00000-0 24007-2 0 9990
2 30129 97.9966 268.2126 0189638 244.8556 176.6674 14.00492296904343
Epoch (UTC): | 05 October 2024 23:32:08 |
Eccentricity: | 0.0189638 |
inclination: | 97.9966° |
perigee height: | 754 km |
apogee height: | 1030 km |
right ascension of ascending node: | 268.2126° |
argument of perigee: | 244.8556° |
revolutions per day: | 14.00492296 |
mean anomaly at epoch: | 176.6674° |
orbit number at epoch: | 90434 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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