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 62111U 26145.60549837 +.00000000 +00000-0 +18838-3 0 00005
2 62111 49.9434 272.0748 0007609 210.3451 149.7060 15.14468219 02
| Epoch (UTC): | 25 May 2026 14:31:55 |
| Eccentricity: | 0.0007609 |
| inclination: | 49.9434° |
| perigee height: | 517 km |
| apogee height: | 528 km |
| right ascension of ascending node: | 272.0748° |
| argument of perigee: | 210.3451° |
| revolutions per day: | 15.14468219 |
| mean anomaly at epoch: | 149.7060° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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