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 66487U 26145.65514351 +.00000000 +00000-0 +63724-3 0 00007
2 66487 43.0016 275.7068 0001328 270.0311 90.0389 15.27595157 06
| Epoch (UTC): | 25 May 2026 15:43:24 |
| Eccentricity: | 0.0001328 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 275.7068° |
| argument of perigee: | 270.0311° |
| revolutions per day: | 15.27595157 |
| mean anomaly at epoch: | 90.0389° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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