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 26040.43653388 +.00000000 +00000-0 +16479-4 0 00009
2 00058 28.3287 67.9566 0164750 229.9328 128.6664 13.46424151 06
| Epoch (UTC): | 09 February 2026 10:28:36 |
| Eccentricity: | 0.0164750 |
| inclination: | 28.3287° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 67.9566° |
| argument of perigee: | 229.9328° |
| revolutions per day: | 13.46424151 |
| mean anomaly at epoch: | 128.6664° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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