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 58902U 24022D 24357.53960210 .00027080 00000-0 10489-2 0 9992
2 58902 97.4586 196.3929 0009084 218.8282 141.2305 15.26099869 49482
| Epoch (UTC): | 22 December 2024 12:57:01 |
| Eccentricity: | 0.0009084 |
| inclination: | 97.4586° |
| perigee height: | 481 km |
| apogee height: | 494 km |
| right ascension of ascending node: | 196.3929° |
| argument of perigee: | 218.8282° |
| revolutions per day: | 15.26099869 |
| mean anomaly at epoch: | 141.2305° |
| orbit number at epoch: | 4948 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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