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 45915U 19079E 24357.82006817 .00005116 00000-0 49282-3 0 9994
2 45915 97.6774 11.9215 0178505 328.2699 30.7853 14.82106306239359
| Epoch (UTC): | 22 December 2024 19:40:53 |
| Eccentricity: | 0.0178505 |
| inclination: | 97.6774° |
| perigee height: | 498 km |
| apogee height: | 747 km |
| right ascension of ascending node: | 11.9215° |
| argument of perigee: | 328.2699° |
| revolutions per day: | 14.82106306 |
| mean anomaly at epoch: | 30.7853° |
| orbit number at epoch: | 23935 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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