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 10096U 26064.21526740 +.00000000 +00000-0 +88701-4 0 00002
2 10096 75.8310 98.3834 0040837 7.0572 353.1186 14.91999864 07
| Epoch (UTC): | 05 March 2026 05:09:59 |
| Eccentricity: | 0.0040837 |
| inclination: | 75.8310° |
| perigee height: | 563 km |
| apogee height: | 620 km |
| right ascension of ascending node: | 98.3834° |
| argument of perigee: | 7.0572° |
| revolutions per day: | 14.91999864 |
| mean anomaly at epoch: | 353.1186° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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