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 63565U 26145.50235135 +.00000000 +00000-0 +49046-3 0 00006
2 63565 42.9959 196.9158 0001527 275.0371 85.0306 15.27588260 00
| Epoch (UTC): | 25 May 2026 12:03:23 |
| Eccentricity: | 0.0001527 |
| inclination: | 42.9959° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 196.9158° |
| argument of perigee: | 275.0371° |
| revolutions per day: | 15.27588260 |
| mean anomaly at epoch: | 85.0306° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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