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 66976U 26145.49215307 +.00000000 +00000-0 +40487-3 0 00002
2 66976 43.0011 309.7333 0001491 269.4209 90.6472 15.27587324 02
| Epoch (UTC): | 25 May 2026 11:48:42 |
| Eccentricity: | 0.0001491 |
| inclination: | 43.0011° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 309.7333° |
| argument of perigee: | 269.4209° |
| revolutions per day: | 15.27587324 |
| mean anomaly at epoch: | 90.6472° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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