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 66508U 26145.36033840 +.00000000 +00000-0 +14089-2 0 00007
2 66508 43.0075 277.7902 0003753 266.7676 93.2746 15.27640337 07
| Epoch (UTC): | 25 May 2026 08:38:53 |
| Eccentricity: | 0.0003753 |
| inclination: | 43.0075° |
| perigee height: | 480 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 277.7902° |
| argument of perigee: | 266.7676° |
| revolutions per day: | 15.27640337 |
| mean anomaly at epoch: | 93.2746° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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