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 59282U 24052C 24358.11228229 .00000369 00000-0 21344-3 0 9993
2 59282 50.0104 274.8148 0006912 60.4446 299.7157 14.27699998 37198
| Epoch (UTC): | 23 December 2024 02:41:41 |
| Eccentricity: | 0.0006912 |
| inclination: | 50.0104° |
| perigee height: | 794 km |
| apogee height: | 804 km |
| right ascension of ascending node: | 274.8148° |
| argument of perigee: | 60.4446° |
| revolutions per day: | 14.27699998 |
| mean anomaly at epoch: | 299.7157° |
| orbit number at epoch: | 3719 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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