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 22676U 93036B 23151.73474231 .00000332 00000-0 12731-3 0 9992
2 22676 74.0402 164.2129 0018386 15.0897 345.0800 14.34304455566744
| Epoch (UTC): | 31 May 2023 17:38:01 |
| Eccentricity: | 0.0018386 |
| inclination: | 74.0402° |
| perigee height: | 764 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 164.2129° |
| argument of perigee: | 15.0897° |
| revolutions per day: | 14.34304455 |
| mean anomaly at epoch: | 345.0800° |
| orbit number at epoch: | 56674 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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