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 63501U 26145.41947701 +.00000000 +00000-0 +80331-3 0 00007
2 63501 53.1566 143.8029 0001056 89.2398 270.8724 15.30192758 02
| Epoch (UTC): | 25 May 2026 10:04:02 |
| Eccentricity: | 0.0001056 |
| inclination: | 53.1566° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 143.8029° |
| argument of perigee: | 89.2398° |
| revolutions per day: | 15.30192758 |
| mean anomaly at epoch: | 270.8724° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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