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 22161U 92064A 23088.21452468 .00000686 00000-0 23085-3 0 9997
2 22161 62.9783 32.3556 0827049 137.3212 229.5178 13.31074632477307
| Epoch (UTC): | 29 March 2023 05:08:54 |
| Eccentricity: | 0.0827049 |
| inclination: | 62.9783° |
| perigee height: | 521 km |
| apogee height: | 1765 km |
| right ascension of ascending node: | 32.3556° |
| argument of perigee: | 137.3212° |
| revolutions per day: | 13.31074632 |
| mean anomaly at epoch: | 229.5178° |
| orbit number at epoch: | 47730 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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