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 63402U 26145.42019845 +.00000000 +00000-0 +54346-3 0 00004
2 63402 43.0024 33.8549 0001447 265.3789 94.6898 15.27593364 07
| Epoch (UTC): | 25 May 2026 10:05:05 |
| Eccentricity: | 0.0001447 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 33.8549° |
| argument of perigee: | 265.3789° |
| revolutions per day: | 15.27593364 |
| mean anomaly at epoch: | 94.6898° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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