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 63500U 26145.38360240 +.00000000 +00000-0 +58431-3 0 00005
2 63500 53.1591 143.5775 0001206 77.9098 282.2038 15.30203651 02
| Epoch (UTC): | 25 May 2026 09:12:23 |
| Eccentricity: | 0.0001206 |
| inclination: | 53.1591° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 143.5775° |
| argument of perigee: | 77.9098° |
| revolutions per day: | 15.30203651 |
| mean anomaly at epoch: | 282.2038° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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