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 63570U 26145.58138933 +.00000000 +00000-0 +57517-3 0 00000
2 63570 43.0003 250.6684 0000277 234.1688 125.9138 15.27593781 09
| Epoch (UTC): | 25 May 2026 13:57:12 |
| Eccentricity: | 0.0000277 |
| inclination: | 43.0003° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 250.6684° |
| argument of perigee: | 234.1688° |
| revolutions per day: | 15.27593781 |
| mean anomaly at epoch: | 125.9138° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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