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 51755C 22016AT 24358.52618056 -.00010758 00000+0 -67468-3 0 3584
2 51755 53.2153 129.5778 0001235 90.5554 223.5185 15.08845894 11
| Epoch (UTC): | 23 December 2024 12:37:42 |
| Eccentricity: | 0.0001235 |
| inclination: | 53.2153° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 129.5778° |
| argument of perigee: | 90.5554° |
| revolutions per day: | 15.08845894 |
| mean anomaly at epoch: | 223.5185° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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