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 53U 60009E 24255.50061052 -.00000018 00000-0 65266-3 0 9998
2 53 47.2770 167.8430 0100806 333.5682 25.9987 12.17347577857016
| Epoch (UTC): | 11 September 2024 12:00:52 |
| Eccentricity: | 0.0100806 |
| inclination: | 47.2770° |
| perigee height: | 1523 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 167.8430° |
| argument of perigee: | 333.5682° |
| revolutions per day: | 12.17347577 |
| mean anomaly at epoch: | 25.9987° |
| orbit number at epoch: | 85701 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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