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 66875U 26145.36634664 +.00000000 +00000-0 +10026-2 0 00002
2 66875 42.9969 270.3149 0001150 284.8845 75.1879 15.27592050 08
| Epoch (UTC): | 25 May 2026 08:47:32 |
| Eccentricity: | 0.0001150 |
| inclination: | 42.9969° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 270.3149° |
| argument of perigee: | 284.8845° |
| revolutions per day: | 15.27592050 |
| mean anomaly at epoch: | 75.1879° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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