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 26088.06180992 +.00000000 +00000-0 +17951-3 0 00007
2 00045 66.6934 212.1288 0253320 218.9758 139.2849 14.35911731 05
| Epoch (UTC): | 29 March 2026 01:29:00 |
| Eccentricity: | 0.0253320 |
| inclination: | 66.6934° |
| perigee height: | 591 km |
| apogee height: | 953 km |
| right ascension of ascending node: | 212.1288° |
| argument of perigee: | 218.9758° |
| revolutions per day: | 14.35911731 |
| mean anomaly at epoch: | 139.2849° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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