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 26048.96307409 +.00000000 +00000-0 +29883-4 0 00008
2 00058 28.3298 24.6939 0164749 300.5337 57.9041 13.46424509 06
| Epoch (UTC): | 17 February 2026 23:06:49 |
| Eccentricity: | 0.0164749 |
| inclination: | 28.3298° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 24.6939° |
| argument of perigee: | 300.5337° |
| revolutions per day: | 13.46424509 |
| mean anomaly at epoch: | 57.9041° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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