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 10707U 76077AC 23085.80734053 -.00000060 00000-0 -22724-3 0 9998
2 10707 102.2535 164.5676 0273662 148.3922 329.6069 11.98139011 11220
| Epoch (UTC): | 26 March 2023 19:22:34 |
| Eccentricity: | 0.0273662 |
| inclination: | 102.2535° |
| perigee height: | 1468 km |
| apogee height: | 1910 km |
| right ascension of ascending node: | 164.5676° |
| argument of perigee: | 148.3922° |
| revolutions per day: | 11.98139011 |
| mean anomaly at epoch: | 329.6069° |
| orbit number at epoch: | 1122 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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