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 29110U 26162.59362984 +.00000000 +00000-0 +13533-2 0 00006
2 29110 98.3259 88.3469 0003418 41.8806 318.2693 15.30342263 03
| Epoch (UTC): | 11 June 2026 14:14:49 |
| Eccentricity: | 0.0003418 |
| inclination: | 98.3259° |
| perigee height: | 472 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 88.3469° |
| argument of perigee: | 41.8806° |
| revolutions per day: | 15.30342263 |
| mean anomaly at epoch: | 318.2693° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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