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 26049.18551299 +.00000000 +00000-0 +28031-4 0 00005
2 00058 28.3298 23.5652 0164746 302.3754 56.0944 13.46424533 05
| Epoch (UTC): | 18 February 2026 04:27:08 |
| Eccentricity: | 0.0164746 |
| inclination: | 28.3298° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 23.5652° |
| argument of perigee: | 302.3754° |
| revolutions per day: | 13.46424533 |
| mean anomaly at epoch: | 56.0944° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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