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 26070.51849323 +.00000000 +00000-0 +80791-4 0 00008
2 10096 75.8307 87.1241 0041029 350.9019 9.1425 14.92010354 04
| Epoch (UTC): | 11 March 2026 12:26:37 |
| Eccentricity: | 0.0041029 |
| inclination: | 75.8307° |
| perigee height: | 563 km |
| apogee height: | 620 km |
| right ascension of ascending node: | 87.1241° |
| argument of perigee: | 350.9019° |
| revolutions per day: | 14.92010354 |
| mean anomaly at epoch: | 9.1425° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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