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 23270.46150042 -.00000080 00000-0 53187-4 0 9996
2 53 47.2752 167.4589 0100741 18.5213 341.9204 12.17312094814376
| Epoch (UTC): | 27 September 2023 11:04:33 |
| Eccentricity: | 0.0100741 |
| inclination: | 47.2752° |
| perigee height: | 1524 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 167.4589° |
| argument of perigee: | 18.5213° |
| revolutions per day: | 12.17312094 |
| mean anomaly at epoch: | 341.9204° |
| orbit number at epoch: | 81437 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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