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 26052.47222184 +.00000000 +00000-0 +00000-0 0 00002
2 35943 0.0351 91.4930 0003357 252.7029 40.1522 1.00270913 03
| Epoch (UTC): | 21 February 2026 11:19:59 |
| Eccentricity: | 0.0003357 |
| inclination: | 0.0351° |
| perigee height: | 35773 km |
| apogee height: | 35801 km |
| right ascension of ascending node: | 91.4930° |
| argument of perigee: | 252.7029° |
| revolutions per day: | 1.00270913 |
| mean anomaly at epoch: | 40.1522° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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