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 63571U 26145.33445029 +.00000000 +00000-0 +42001-3 0 00003
2 63571 42.9964 248.7246 0001080 220.1151 139.9621 15.27595695 07
| Epoch (UTC): | 25 May 2026 08:01:36 |
| Eccentricity: | 0.0001080 |
| inclination: | 42.9964° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 248.7246° |
| argument of perigee: | 220.1151° |
| revolutions per day: | 15.27595695 |
| mean anomaly at epoch: | 139.9621° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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