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 35942U 26136.46701632 +.00000000 +00000-0 +00000-0 0 00003
2 35942 1.7333 83.3796 0004533 37.9482 220.0833 1.00221129 02
| Epoch (UTC): | 16 May 2026 11:12:30 |
| Eccentricity: | 0.0004533 |
| inclination: | 1.7333° |
| perigee height: | 35782 km |
| apogee height: | 35820 km |
| right ascension of ascending node: | 83.3796° |
| argument of perigee: | 37.9482° |
| revolutions per day: | 1.00221129 |
| mean anomaly at epoch: | 220.0833° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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