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 28352U 26065.89912529 +.00000000 +00000-0 -82120-4 0 00005
2 28352 71.0013 313.3011 0012147 287.3551 72.6241 14.12145918 00
| Epoch (UTC): | 06 March 2026 21:34:44 |
| Eccentricity: | 0.0012147 |
| inclination: | 71.0013° |
| perigee height: | 843 km |
| apogee height: | 861 km |
| right ascension of ascending node: | 313.3011° |
| argument of perigee: | 287.3551° |
| revolutions per day: | 14.12145918 |
| mean anomaly at epoch: | 72.6241° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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