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 62049U 26145.57599528 +.00000000 +00000-0 +45649-3 0 00003
2 62049 43.0003 182.1709 0001546 270.4171 89.6503 15.27598940 00
| Epoch (UTC): | 25 May 2026 13:49:25 |
| Eccentricity: | 0.0001546 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 182.1709° |
| argument of perigee: | 270.4171° |
| revolutions per day: | 15.27598940 |
| mean anomaly at epoch: | 89.6503° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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