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 00016U 26153.89818230 +.00000000 +00000-0 +22016-3 0 00000
2 00016 34.2646 346.3814 2017175 60.1797 318.4127 10.49591345 03
| Epoch (UTC): | 02 June 2026 21:33:22 |
| Eccentricity: | 0.2017175 |
| inclination: | 34.2646° |
| perigee height: | 656 km |
| apogee height: | 4211 km |
| right ascension of ascending node: | 346.3814° |
| argument of perigee: | 60.1797° |
| revolutions per day: | 10.49591345 |
| mean anomaly at epoch: | 318.4127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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