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 63569U 26145.63921861 +.00000000 +00000-0 +11824-2 0 00004
2 63569 42.9999 251.1051 0001809 275.4371 84.6274 15.27599946 03
| Epoch (UTC): | 25 May 2026 15:20:28 |
| Eccentricity: | 0.0001809 |
| inclination: | 42.9999° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 251.1051° |
| argument of perigee: | 275.4371° |
| revolutions per day: | 15.27599946 |
| mean anomaly at epoch: | 84.6274° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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