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 44058U 26145.25142175 +.00000000 +00000-0 +97664-4 0 00005
2 44058 87.9106 233.3345 0001634 99.1897 260.9419 13.16593225 02
| Epoch (UTC): | 25 May 2026 06:02:02 |
| Eccentricity: | 0.0001634 |
| inclination: | 87.9106° |
| perigee height: | 1197 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.3345° |
| argument of perigee: | 99.1897° |
| revolutions per day: | 13.16593225 |
| mean anomaly at epoch: | 260.9419° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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