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 44882U 26145.58163865 +.00000000 +00000-0 +44941-3 0 00004
2 44882 97.7926 240.1626 0015725 100.4781 259.8217 15.04894783 03
| Epoch (UTC): | 25 May 2026 13:57:33 |
| Eccentricity: | 0.0015725 |
| inclination: | 97.7926° |
| perigee height: | 541 km |
| apogee height: | 563 km |
| right ascension of ascending node: | 240.1626° |
| argument of perigee: | 100.4781° |
| revolutions per day: | 15.04894783 |
| mean anomaly at epoch: | 259.8217° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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