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 44475U 26128.16919860 +.00000000 +00000-0 +00000-0 0 00006
2 44475 0.0172 237.7879 0001275 172.2749 19.3596 1.00274219 05
| Epoch (UTC): | 08 May 2026 04:03:38 |
| Eccentricity: | 0.0001275 |
| inclination: | 0.0172° |
| perigee height: | 35781 km |
| apogee height: | 35791 km |
| right ascension of ascending node: | 237.7879° |
| argument of perigee: | 172.2749° |
| revolutions per day: | 1.00274219 |
| mean anomaly at epoch: | 19.3596° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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