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 63201U 26145.33445889 +.00000000 +00000-0 +49872-3 0 00000
2 63201 43.0030 12.4945 0000883 293.6844 66.3915 15.27615074 02
| Epoch (UTC): | 25 May 2026 08:01:37 |
| Eccentricity: | 0.0000883 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 12.4945° |
| argument of perigee: | 293.6844° |
| revolutions per day: | 15.27615074 |
| mean anomaly at epoch: | 66.3915° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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