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 62016U 26145.63153124 +.00000000 +00000-0 +15936-2 0 00007
2 62016 53.1582 21.6803 0001606 96.4701 263.6500 15.69765581 06
| Epoch (UTC): | 25 May 2026 15:09:24 |
| Eccentricity: | 0.0001606 |
| inclination: | 53.1582° |
| perigee height: | 358 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 21.6803° |
| argument of perigee: | 96.4701° |
| revolutions per day: | 15.69765581 |
| mean anomaly at epoch: | 263.6500° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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