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 62843U 26145.33526977 +.00000000 +00000-0 +68877-3 0 00005
2 62843 43.0028 16.0632 0001132 267.9140 92.1582 15.27601845 02
| Epoch (UTC): | 25 May 2026 08:02:47 |
| Eccentricity: | 0.0001132 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 16.0632° |
| argument of perigee: | 267.9140° |
| revolutions per day: | 15.27601845 |
| mean anomaly at epoch: | 92.1582° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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