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 66157U 26145.48085414 +.00000000 +00000-0 +79424-3 0 00009
2 66157 53.1601 65.5454 0001017 74.1099 286.0016 15.34409736 06
| Epoch (UTC): | 25 May 2026 11:32:25 |
| Eccentricity: | 0.0001017 |
| inclination: | 53.1601° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 65.5454° |
| argument of perigee: | 74.1099° |
| revolutions per day: | 15.34409736 |
| mean anomaly at epoch: | 286.0016° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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