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 00705U 63049C 22223.53614632 .00000065 00000-0 90655-4 0 9995
2 00705 89.9029 82.7869 0033366 342.4685 76.9478 13.47394419882817
| Epoch (UTC): | 11 August 2022 12:52:03 |
| Eccentricity: | 0.0033366 |
| inclination: | 89.9029° |
| perigee height: | 1057 km |
| apogee height: | 1107 km |
| right ascension of ascending node: | 82.7869° |
| argument of perigee: | 342.4685° |
| revolutions per day: | 13.47394419 |
| mean anomaly at epoch: | 76.9478° |
| orbit number at epoch: | 88281 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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