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 66434U 26145.51210887 +.00000000 +00000-0 +70177-3 0 00001
2 66434 42.9993 200.2018 0001526 268.2898 91.7779 15.27620433 04
| Epoch (UTC): | 25 May 2026 12:17:26 |
| Eccentricity: | 0.0001526 |
| inclination: | 42.9993° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 200.2018° |
| argument of perigee: | 268.2898° |
| revolutions per day: | 15.27620433 |
| mean anomaly at epoch: | 91.7779° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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