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 02016U 26106.74525006 +.00000000 +00000-0 +10335-3 0 00001
2 02016 34.0889 227.3126 1157870 12.9942 349.8045 12.66484218 07
| Epoch (UTC): | 16 April 2026 17:53:09 |
| Eccentricity: | 0.1157870 |
| inclination: | 34.0889° |
| perigee height: | 496 km |
| apogee height: | 2296 km |
| right ascension of ascending node: | 227.3126° |
| argument of perigee: | 12.9942° |
| revolutions per day: | 12.66484218 |
| mean anomaly at epoch: | 349.8045° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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