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 22184.87992448 .00000021 00000-0 39657-4 0 9994
2 26931 67.0518 15.9985 0007381 261.2719 98.7547 14.30712981 83753
| Epoch (UTC): | 03 July 2022 21:07:05 |
| Eccentricity: | 0.0007381 |
| inclination: | 67.0518° |
| perigee height: | 784 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 15.9985° |
| argument of perigee: | 261.2719° |
| revolutions per day: | 14.30712981 |
| mean anomaly at epoch: | 98.7547° |
| orbit number at epoch: | 8375 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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