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 26106.80544372 +.00000000 +00000-0 +13423-3 0 00002
2 42829 97.4205 266.8401 0016716 306.0715 53.8963 15.04575174 07
| Epoch (UTC): | 16 April 2026 19:19:50 |
| Eccentricity: | 0.0016716 |
| inclination: | 97.4205° |
| perigee height: | 541 km |
| apogee height: | 564 km |
| right ascension of ascending node: | 266.8401° |
| argument of perigee: | 306.0715° |
| revolutions per day: | 15.04575174 |
| mean anomaly at epoch: | 53.8963° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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