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 42836U 26106.16297605 +.00000000 +00000-0 +13836-3 0 00001
2 42836 97.4192 270.1971 0003041 328.4392 31.6654 15.08433003 05
| Epoch (UTC): | 16 April 2026 03:54:41 |
| Eccentricity: | 0.0003041 |
| inclination: | 97.4192° |
| perigee height: | 539 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 270.1971° |
| argument of perigee: | 328.4392° |
| revolutions per day: | 15.08433003 |
| mean anomaly at epoch: | 31.6654° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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