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 44881U 19093C 22142.17407797 .00000950 00000-0 12721-3 0 9990
2 44881 97.8926 221.7598 0013616 272.1456 87.8217 14.81696281130885
| Epoch (UTC): | 22 May 2022 04:10:40 |
| Eccentricity: | 0.0013616 |
| inclination: | 97.8926° |
| perigee height: | 614 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 221.7598° |
| argument of perigee: | 272.1456° |
| revolutions per day: | 14.81696281 |
| mean anomaly at epoch: | 87.8217° |
| orbit number at epoch: | 13088 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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