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 26931U 01043C 22278.83285265 .00000179 00000-0 10013-3 0 9994
2 26931 67.0499 133.4849 0005657 258.7847 101.2618 14.30740458 97195
| Epoch (UTC): | 05 October 2022 19:59:18 |
| Eccentricity: | 0.0005657 |
| inclination: | 67.0499° |
| perigee height: | 785 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 133.4849° |
| argument of perigee: | 258.7847° |
| revolutions per day: | 14.30740458 |
| mean anomaly at epoch: | 101.2618° |
| orbit number at epoch: | 9719 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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