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 66527U 26145.46813338 +.00000000 +00000-0 +87354-3 0 00003
2 66527 43.0001 204.5093 0001589 281.0861 78.9812 15.27590074 03
| Epoch (UTC): | 25 May 2026 11:14:06 |
| Eccentricity: | 0.0001589 |
| inclination: | 43.0001° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 204.5093° |
| argument of perigee: | 281.0861° |
| revolutions per day: | 15.27590074 |
| mean anomaly at epoch: | 78.9812° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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