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 26069U 00006A 23151.89230230 .00000275 00000-0 17132-3 0 9999
2 26069 70.9927 122.9468 0011610 184.1587 175.9440 14.13542249466757
| Epoch (UTC): | 31 May 2023 21:24:54 |
| Eccentricity: | 0.0011610 |
| inclination: | 70.9927° |
| perigee height: | 839 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 122.9468° |
| argument of perigee: | 184.1587° |
| revolutions per day: | 14.13542249 |
| mean anomaly at epoch: | 175.9440° |
| orbit number at epoch: | 46675 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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