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 63071U 26145.49521170 +.00000000 +00000-0 +89840-3 0 00009
2 63071 42.9997 70.0684 0000820 49.6493 310.4431 15.27583042 02
| Epoch (UTC): | 25 May 2026 11:53:06 |
| Eccentricity: | 0.0000820 |
| inclination: | 42.9997° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 70.0684° |
| argument of perigee: | 49.6493° |
| revolutions per day: | 15.27583042 |
| mean anomaly at epoch: | 310.4431° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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