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 05918U 72022B 22141.61199204 .00000037 00000-0 14960-4 0 9992
2 05918 81.2399 25.1202 0057691 311.6750 47.9488 14.05913123570562
| Epoch (UTC): | 21 May 2022 14:41:16 |
| Eccentricity: | 0.0057691 |
| inclination: | 81.2399° |
| perigee height: | 831 km |
| apogee height: | 915 km |
| right ascension of ascending node: | 25.1202° |
| argument of perigee: | 311.6750° |
| revolutions per day: | 14.05913123 |
| mean anomaly at epoch: | 47.9488° |
| orbit number at epoch: | 57056 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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