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 26694U 01005A 23290.87609137 0.00000000 00000-0 00000-0 0 03
2 26694 10.6817 36.7564 0008883 109.5484 250.5596 0.98731991 00
| Epoch (UTC): | 17 October 2023 21:01:34 |
| Eccentricity: | 0.0008883 |
| inclination: | 10.6817° |
| perigee height: | 36185 km |
| apogee height: | 36261 km |
| right ascension of ascending node: | 36.7564° |
| argument of perigee: | 109.5484° |
| revolutions per day: | 0.98731991 |
| mean anomaly at epoch: | 250.5596° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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