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 63561U 26145.44210500 +.00000000 +00000-0 +27145-3 0 00000
2 63561 42.9991 197.3497 0001171 265.9971 94.0747 15.27574694 07
| Epoch (UTC): | 25 May 2026 10:36:37 |
| Eccentricity: | 0.0001171 |
| inclination: | 42.9991° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 197.3497° |
| argument of perigee: | 265.9971° |
| revolutions per day: | 15.27574694 |
| mean anomaly at epoch: | 94.0747° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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