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 00045U 60007A 24254.72272603 .00001880 00000-0 47693-3 0 9997
2 00045 66.6919 263.7408 0259379 269.4941 87.6437 14.34912565287549
| Epoch (UTC): | 10 September 2024 17:20:43 |
| Eccentricity: | 0.0259379 |
| inclination: | 66.6919° |
| perigee height: | 590 km |
| apogee height: | 961 km |
| right ascension of ascending node: | 263.7408° |
| argument of perigee: | 269.4941° |
| revolutions per day: | 14.34912565 |
| mean anomaly at epoch: | 87.6437° |
| orbit number at epoch: | 28754 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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