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 26161.54742635 +.00000000 +00000-0 +12027-2 0 00002
2 29110 98.3256 87.1743 0003539 43.2599 316.8916 15.30256989 02
| Epoch (UTC): | 10 June 2026 13:08:17 |
| Eccentricity: | 0.0003539 |
| inclination: | 98.3256° |
| perigee height: | 473 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 87.1743° |
| argument of perigee: | 43.2599° |
| revolutions per day: | 15.30256989 |
| mean anomaly at epoch: | 316.8916° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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