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 35943U 26103.17309419 +.00000000 +00000-0 +00000-0 0 00003
2 35943 0.0799 81.5209 0003927 317.8447 287.3423 1.00273646 09
| Epoch (UTC): | 13 April 2026 04:09:15 |
| Eccentricity: | 0.0003927 |
| inclination: | 0.0799° |
| perigee height: | 35770 km |
| apogee height: | 35803 km |
| right ascension of ascending node: | 81.5209° |
| argument of perigee: | 317.8447° |
| revolutions per day: | 1.00273646 |
| mean anomaly at epoch: | 287.3423° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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