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 63061U 26145.65523110 +.00000000 +00000-0 +12352-2 0 00005
2 63061 43.0022 271.5825 0003960 288.8326 71.2112 15.70840249 08
| Epoch (UTC): | 25 May 2026 15:43:31 |
| Eccentricity: | 0.0003960 |
| inclination: | 43.0022° |
| perigee height: | 354 km |
| apogee height: | 359 km |
| right ascension of ascending node: | 271.5825° |
| argument of perigee: | 288.8326° |
| revolutions per day: | 15.70840249 |
| mean anomaly at epoch: | 71.2112° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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