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 26880U 01033A 23344.15558434 -.00000277 00000-0 00000-0 0 9999
2 26880 11.9172 22.4753 0000210 192.3374 230.6716 1.00267246 23741
| Epoch (UTC): | 10 December 2023 03:44:02 |
| Eccentricity: | 0.0000210 |
| inclination: | 11.9172° |
| perigee height: | 35786 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 22.4753° |
| argument of perigee: | 192.3374° |
| revolutions per day: | 1.00267246 |
| mean anomaly at epoch: | 230.6716° |
| orbit number at epoch: | 2374 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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