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 40677U 95015FR 22216.79145043 .00000163 00000-0 86393-4 0 9993
2 40677 98.6607 232.9383 0051643 69.7437 290.9283 14.25350772379038
| Epoch (UTC): | 04 August 2022 18:59:41 |
| Eccentricity: | 0.0051643 |
| inclination: | 98.6607° |
| perigee height: | 770 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 232.9383° |
| argument of perigee: | 69.7437° |
| revolutions per day: | 14.25350772 |
| mean anomaly at epoch: | 290.9283° |
| orbit number at epoch: | 37903 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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