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 63581U 26145.59214703 +.00000000 +00000-0 +87512-3 0 00001
2 63581 42.9982 247.2183 0001182 268.9556 91.1160 15.27581991 05
| Epoch (UTC): | 25 May 2026 14:12:41 |
| Eccentricity: | 0.0001182 |
| inclination: | 42.9982° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 247.2183° |
| argument of perigee: | 268.9556° |
| revolutions per day: | 15.27581991 |
| mean anomaly at epoch: | 91.1160° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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