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 62741U 26145.54375242 +.00000000 +00000-0 +39045-3 0 00007
2 62741 43.0034 80.1509 0000823 269.8490 90.2267 15.27585331 06
| Epoch (UTC): | 25 May 2026 13:03:00 |
| Eccentricity: | 0.0000823 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 80.1509° |
| argument of perigee: | 269.8490° |
| revolutions per day: | 15.27585331 |
| mean anomaly at epoch: | 90.2267° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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