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 66928U 26145.02236106 +.00000000 +00000-0 +11576-2 0 00004
2 66928 53.1606 3.8966 0001074 87.7701 272.3424 15.34405060 00
| Epoch (UTC): | 25 May 2026 00:32:11 |
| Eccentricity: | 0.0001074 |
| inclination: | 53.1606° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 3.8966° |
| argument of perigee: | 87.7701° |
| revolutions per day: | 15.34405060 |
| mean anomaly at epoch: | 272.3424° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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