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 66387U 26145.39475203 +.00000000 +00000-0 +40567-3 0 00009
2 66387 53.1597 219.5836 0000455 125.4037 234.7008 15.34402377 02
| Epoch (UTC): | 25 May 2026 09:28:26 |
| Eccentricity: | 0.0000455 |
| inclination: | 53.1597° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 219.5836° |
| argument of perigee: | 125.4037° |
| revolutions per day: | 15.34402377 |
| mean anomaly at epoch: | 234.7008° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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