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 66477U 26145.48631032 +.00000000 +00000-0 +53141-3 0 00005
2 66477 42.9995 222.2671 0001633 269.8971 90.1694 15.27611300 02
| Epoch (UTC): | 25 May 2026 11:40:17 |
| Eccentricity: | 0.0001633 |
| inclination: | 42.9995° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 222.2671° |
| argument of perigee: | 269.8971° |
| revolutions per day: | 15.27611300 |
| mean anomaly at epoch: | 90.1694° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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