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 26159.52024838 +.00000000 +00000-0 +13872-2 0 00004
2 29110 98.3256 84.9036 0003888 46.8534 313.3028 15.30105377 07
| Epoch (UTC): | 08 June 2026 12:29:09 |
| Eccentricity: | 0.0003888 |
| inclination: | 98.3256° |
| perigee height: | 473 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 84.9036° |
| argument of perigee: | 46.8534° |
| revolutions per day: | 15.30105377 |
| mean anomaly at epoch: | 313.3028° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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