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 26140.67933634 +.00000000 +00000-0 +32997-4 0 00004
2 00058 28.3284 279.3145 0164932 340.0129 19.4015 13.46429455 00
| Epoch (UTC): | 20 May 2026 16:18:14 |
| Eccentricity: | 0.0164932 |
| inclination: | 28.3284° |
| perigee height: | 962 km |
| apogee height: | 1209 km |
| right ascension of ascending node: | 279.3145° |
| argument of perigee: | 340.0129° |
| revolutions per day: | 13.46429455 |
| mean anomaly at epoch: | 19.4015° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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