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 26039.14767140 +.00000000 +00000-0 +44124-3 0 00006
2 05118 81.2347 88.4555 0017489 38.6435 321.6064 15.58789924 05
| Epoch (UTC): | 08 February 2026 03:32:38 |
| Eccentricity: | 0.0017489 |
| inclination: | 81.2347° |
| perigee height: | 379 km |
| apogee height: | 403 km |
| right ascension of ascending node: | 88.4555° |
| argument of perigee: | 38.6435° |
| revolutions per day: | 15.58789924 |
| mean anomaly at epoch: | 321.6064° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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