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 00045U 26149.14589138 +.00000000 +00000-0 +70476-4 0 00001
2 00045 66.6945 50.5639 0247825 174.7971 185.5799 14.35952844 08
| Epoch (UTC): | 29 May 2026 03:30:05 |
| Eccentricity: | 0.0247825 |
| inclination: | 66.6945° |
| perigee height: | 595 km |
| apogee height: | 949 km |
| right ascension of ascending node: | 50.5639° |
| argument of perigee: | 174.7971° |
| revolutions per day: | 14.35952844 |
| mean anomaly at epoch: | 185.5799° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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