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 44881U 26088.20837174 +.00000000 +00000-0 +79273-4 0 00006
2 44881 97.7578 162.3812 0013481 356.3806 3.7310 14.86379835 09
| Epoch (UTC): | 29 March 2026 05:00:03 |
| Eccentricity: | 0.0013481 |
| inclination: | 97.7578° |
| perigee height: | 600 km |
| apogee height: | 619 km |
| right ascension of ascending node: | 162.3812° |
| argument of perigee: | 356.3806° |
| revolutions per day: | 14.86379835 |
| mean anomaly at epoch: | 3.7310° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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