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 22826U 93061D 23088.34242248 .00000316 00000-0 13866-3 0 9996
2 22826 98.8466 129.7725 0007903 289.1956 70.8370 14.30630329539143
| Epoch (UTC): | 29 March 2023 08:13:05 |
| Eccentricity: | 0.0007903 |
| inclination: | 98.8466° |
| perigee height: | 784 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 129.7725° |
| argument of perigee: | 289.1956° |
| revolutions per day: | 14.30630329 |
| mean anomaly at epoch: | 70.8370° |
| orbit number at epoch: | 53914 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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