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 43775U 26111.35918132 +.00000000 +00000-0 +16902-3 0 00003
2 43775 97.4258 157.3777 0006523 148.5456 211.6165 15.09757637 01
| Epoch (UTC): | 21 April 2026 08:37:13 |
| Eccentricity: | 0.0006523 |
| inclination: | 97.4258° |
| perigee height: | 532 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 157.3777° |
| argument of perigee: | 148.5456° |
| revolutions per day: | 15.09757637 |
| mean anomaly at epoch: | 211.6165° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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