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 05010U 71015D 22226.54215013 .00000703 00000-0 24411-3 0 9990
2 05010 65.8436 157.4756 0697057 229.8465 123.9526 13.53288522457727
| Epoch (UTC): | 14 August 2022 13:00:41 |
| Eccentricity: | 0.0697057 |
| inclination: | 65.8436° |
| perigee height: | 541 km |
| apogee height: | 1578 km |
| right ascension of ascending node: | 157.4756° |
| argument of perigee: | 229.8465° |
| revolutions per day: | 13.53288522 |
| mean anomaly at epoch: | 123.9526° |
| orbit number at epoch: | 45772 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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