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 66873U 26145.37020036 +.00000000 +00000-0 +77782-3 0 00006
2 66873 42.9987 270.3459 0001008 282.1511 77.9227 15.27597533 01
| Epoch (UTC): | 25 May 2026 08:53:05 |
| Eccentricity: | 0.0001008 |
| inclination: | 42.9987° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 270.3459° |
| argument of perigee: | 282.1511° |
| revolutions per day: | 15.27597533 |
| mean anomaly at epoch: | 77.9227° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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