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 42829U 26087.98370547 +.00000000 +00000-0 +33255-3 0 00005
2 42829 97.4186 248.7638 0017896 12.3109 347.8551 15.04440964 07
| Epoch (UTC): | 28 March 2026 23:36:32 |
| Eccentricity: | 0.0017896 |
| inclination: | 97.4186° |
| perigee height: | 541 km |
| apogee height: | 566 km |
| right ascension of ascending node: | 248.7638° |
| argument of perigee: | 12.3109° |
| revolutions per day: | 15.04440964 |
| mean anomaly at epoch: | 347.8551° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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