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 62393U 26145.59249590 +.00000000 +00000-0 +15901-2 0 00005
2 62393 44.9627 353.0907 0017115 255.6496 104.2508 15.81999580 01
| Epoch (UTC): | 25 May 2026 14:13:11 |
| Eccentricity: | 0.0017115 |
| inclination: | 44.9627° |
| perigee height: | 313 km |
| apogee height: | 336 km |
| right ascension of ascending node: | 353.0907° |
| argument of perigee: | 255.6496° |
| revolutions per day: | 15.81999580 |
| mean anomaly at epoch: | 104.2508° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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