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 66307U 26145.53423884 +.00000000 +00000-0 +55656-3 0 00000
2 66307 45.3862 236.5849 0012803 294.4672 65.4881 15.26382147 08
| Epoch (UTC): | 25 May 2026 12:49:18 |
| Eccentricity: | 0.0012803 |
| inclination: | 45.3862° |
| perigee height: | 478 km |
| apogee height: | 495 km |
| right ascension of ascending node: | 236.5849° |
| argument of perigee: | 294.4672° |
| revolutions per day: | 15.26382147 |
| mean anomaly at epoch: | 65.4881° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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