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 41286U 00055GN 22222.40023512 .00012536 00000-0 40411-2 0 9997
2 41286 98.8983 13.5537 0049787 321.7008 38.0646 14.38636489344974
| Epoch (UTC): | 10 August 2022 09:36:20 |
| Eccentricity: | 0.0049787 |
| inclination: | 98.8983° |
| perigee height: | 727 km |
| apogee height: | 798 km |
| right ascension of ascending node: | 13.5537° |
| argument of perigee: | 321.7008° |
| revolutions per day: | 14.38636489 |
| mean anomaly at epoch: | 38.0646° |
| orbit number at epoch: | 34497 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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