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 24251.14976593 -.00000095 00000-0 -10787-3 0 9993
2 53 47.2765 181.2622 0100949 320.6579 38.6909 12.17347045856488
| Epoch (UTC): | 07 September 2024 03:35:39 |
| Eccentricity: | 0.0100949 |
| inclination: | 47.2765° |
| perigee height: | 1523 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 181.2622° |
| argument of perigee: | 320.6579° |
| revolutions per day: | 12.17347045 |
| mean anomaly at epoch: | 38.6909° |
| orbit number at epoch: | 85648 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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