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 is defined by the following mean orbital elements,
1 66953U 26145.47735845 +.00000000 +00000-0 +54331-4 0 00003
2 66953 86.4915 290.0430 0001588 108.4564 251.6743 13.24410710 03
| Epoch (UTC): | 25 May 2026 11:27:23 |
| Eccentricity: | 0.0001588 |
| inclination: | 86.4915° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 290.0430° |
| argument of perigee: | 108.4564° |
| revolutions per day: | 13.24410710 |
| mean anomaly at epoch: | 251.6743° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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