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 23270.45578854 .00000337 00000-0 15934-3 0 9997
2 26931 67.0500 292.7471 0007264 258.4880 101.5406 14.30990441148372
| Epoch (UTC): | 27 September 2023 10:56:20 |
| Eccentricity: | 0.0007264 |
| inclination: | 67.0500° |
| perigee height: | 783 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 292.7471° |
| argument of perigee: | 258.4880° |
| revolutions per day: | 14.30990441 |
| mean anomaly at epoch: | 101.5406° |
| orbit number at epoch: | 14837 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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