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 62116U 26145.49222086 +.00000000 +00000-0 +50109-3 0 00008
2 62116 43.0042 62.5514 0000920 266.2616 93.8131 15.27590592 04
| Epoch (UTC): | 25 May 2026 11:48:47 |
| Eccentricity: | 0.0000920 |
| inclination: | 43.0042° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 62.5514° |
| argument of perigee: | 266.2616° |
| revolutions per day: | 15.27590592 |
| mean anomaly at epoch: | 93.8131° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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