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 25347.78395584 .00000285 00000-0 13745-3 0 9997
2 26931 67.0515 3.7782 0007426 269.9261 90.0990 14.31855546263907
| Epoch (UTC): | 13 December 2025 18:48:53 |
| Eccentricity: | 0.0007426 |
| inclination: | 67.0515° |
| perigee height: | 780 km |
| apogee height: | 791 km |
| right ascension of ascending node: | 3.7782° |
| argument of perigee: | 269.9261° |
| revolutions per day: | 14.31855546 |
| mean anomaly at epoch: | 90.0990° |
| orbit number at epoch: | 26390 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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