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 26106.64776227 +.00000000 +00000-0 +18563-4 0 00009
2 00058 28.3264 91.9903 0164917 58.2485 303.4017 13.46428308 08
| Epoch (UTC): | 16 April 2026 15:32:46 |
| Eccentricity: | 0.0164917 |
| inclination: | 28.3264° |
| perigee height: | 962 km |
| apogee height: | 1209 km |
| right ascension of ascending node: | 91.9903° |
| argument of perigee: | 58.2485° |
| revolutions per day: | 13.46428308 |
| mean anomaly at epoch: | 303.4017° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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