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 22178.77556577 .00000492 00000-0 68973-4 0 9998
2 44881 97.8925 257.8359 0015705 147.9403 212.2763 14.81739999136308
| Epoch (UTC): | 27 June 2022 18:36:48 |
| Eccentricity: | 0.0015705 |
| inclination: | 97.8925° |
| perigee height: | 613 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 257.8359° |
| argument of perigee: | 147.9403° |
| revolutions per day: | 14.81739999 |
| mean anomaly at epoch: | 212.2763° |
| orbit number at epoch: | 13630 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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