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 42521U 70025SB 24355.53883857 .00001251 00000-0 12600-2 0 9994
2 42521 99.9951 18.9906 0015335 128.1378 232.1157 13.79551826 88721
| Epoch (UTC): | 20 December 2024 12:55:55 |
| Eccentricity: | 0.0015335 |
| inclination: | 99.9951° |
| perigee height: | 954 km |
| apogee height: | 977 km |
| right ascension of ascending node: | 18.9906° |
| argument of perigee: | 128.1378° |
| revolutions per day: | 13.79551826 |
| mean anomaly at epoch: | 232.1157° |
| orbit number at epoch: | 8872 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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