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 58316U 23174BN 24358.14576994 .00026116 00000-0 94245-3 0 9990
2 58316 97.4358 71.5056 0009178 278.2341 81.7857 15.28447717 62490
Epoch (UTC): | 23 December 2024 03:29:54 |
Eccentricity: | 0.0009178 |
inclination: | 97.4358° |
perigee height: | 474 km |
apogee height: | 487 km |
right ascension of ascending node: | 71.5056° |
argument of perigee: | 278.2341° |
revolutions per day: | 15.28447717 |
mean anomaly at epoch: | 81.7857° |
orbit number at epoch: | 6249 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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