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 05118U 26039.46863446 +.00000000 +00000-0 +44786-3 0 00001
2 05118 81.2348 88.0605 0017458 37.5491 322.6976 15.58812170 07
| Epoch (UTC): | 08 February 2026 11:14:50 |
| Eccentricity: | 0.0017458 |
| inclination: | 81.2348° |
| perigee height: | 379 km |
| apogee height: | 403 km |
| right ascension of ascending node: | 88.0605° |
| argument of perigee: | 37.5491° |
| revolutions per day: | 15.58812170 |
| mean anomaly at epoch: | 322.6976° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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