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 44886U 26145.65378463 +.00000000 +00000-0 +54411-3 0 00001
2 44886 97.7993 233.9327 0012979 135.7616 224.4645 14.95027623 08
| Epoch (UTC): | 25 May 2026 15:41:26 |
| Eccentricity: | 0.0012979 |
| inclination: | 97.7993° |
| perigee height: | 573 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 233.9327° |
| argument of perigee: | 135.7616° |
| revolutions per day: | 14.95027623 |
| mean anomaly at epoch: | 224.4645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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