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 00058U 26046.14554553 +.00000000 +00000-0 +17887-4 0 00001
2 00058 28.3296 38.9893 0164753 277.2030 80.9812 13.46424370 04
| Epoch (UTC): | 15 February 2026 03:29:35 |
| Eccentricity: | 0.0164753 |
| inclination: | 28.3296° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 38.9893° |
| argument of perigee: | 277.2030° |
| revolutions per day: | 13.46424370 |
| mean anomaly at epoch: | 80.9812° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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