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 27691U 03008A 23088.04569389 .00000049 00000-0 00000-0 0 9994
2 27691 8.6052 52.7333 0001473 295.7443 84.0881 1.00273237 21164
| Epoch (UTC): | 29 March 2023 01:05:47 |
| Eccentricity: | 0.0001473 |
| inclination: | 8.6052° |
| perigee height: | 35779 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 52.7333° |
| argument of perigee: | 295.7443° |
| revolutions per day: | 1.00273237 |
| mean anomaly at epoch: | 84.0881° |
| orbit number at epoch: | 2116 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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