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 63016U 26145.55095727 +.00000000 +00000-0 +22717-2 0 00008
2 63016 42.9983 91.9012 0001820 309.4875 50.5831 15.70995085 03
| Epoch (UTC): | 25 May 2026 13:13:22 |
| Eccentricity: | 0.0001820 |
| inclination: | 42.9983° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 91.9012° |
| argument of perigee: | 309.4875° |
| revolutions per day: | 15.70995085 |
| mean anomaly at epoch: | 50.5831° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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