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 66528U 26145.44243272 +.00000000 +00000-0 +57469-3 0 00000
2 66528 42.9969 204.3108 0000190 196.0857 163.9989 15.27597163 03
| Epoch (UTC): | 25 May 2026 10:37:06 |
| Eccentricity: | 0.0000190 |
| inclination: | 42.9969° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 204.3108° |
| argument of perigee: | 196.0857° |
| revolutions per day: | 15.27597163 |
| mean anomaly at epoch: | 163.9989° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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