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 66167U 26145.08372560 +.00000000 +00000-0 +68956-3 0 00005
2 66167 53.1588 67.3213 0000958 79.8170 280.2941 15.34403254 01
| Epoch (UTC): | 25 May 2026 02:00:33 |
| Eccentricity: | 0.0000958 |
| inclination: | 53.1588° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 67.3213° |
| argument of perigee: | 79.8170° |
| revolutions per day: | 15.34403254 |
| mean anomaly at epoch: | 280.2941° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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