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 26053.75706550 +.00000000 +00000-0 +24703-3 0 00002
2 02016 34.0875 92.3060 1157840 43.2280 325.3591 12.66401708 06
| Epoch (UTC): | 22 February 2026 18:10:10 |
| Eccentricity: | 0.1157840 |
| inclination: | 34.0875° |
| perigee height: | 496 km |
| apogee height: | 2297 km |
| right ascension of ascending node: | 92.3060° |
| argument of perigee: | 43.2280° |
| revolutions per day: | 12.66401708 |
| mean anomaly at epoch: | 325.3591° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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