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 26048.29575939 +.00000000 +00000-0 +26926-4 0 00004
2 00058 28.3298 28.0797 0164750 295.0082 63.3437 13.46424490 02
| Epoch (UTC): | 17 February 2026 07:05:53 |
| Eccentricity: | 0.0164750 |
| inclination: | 28.3298° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 28.0797° |
| argument of perigee: | 295.0082° |
| revolutions per day: | 13.46424490 |
| mean anomaly at epoch: | 63.3437° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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