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 26069.51266253 +.00000000 +00000-0 +81771-4 0 00000
2 10096 75.8307 88.9208 0040995 353.4738 6.5915 14.92008563 07
| Epoch (UTC): | 10 March 2026 12:18:14 |
| Eccentricity: | 0.0040995 |
| inclination: | 75.8307° |
| perigee height: | 563 km |
| apogee height: | 620 km |
| right ascension of ascending node: | 88.9208° |
| argument of perigee: | 353.4738° |
| revolutions per day: | 14.92008563 |
| mean anomaly at epoch: | 6.5915° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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