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 62654U 26145.49005774 +.00000000 +00000-0 +16657-3 0 00008
2 62654 97.4055 226.2573 0002852 58.0263 302.1251 15.23748476 04
| Epoch (UTC): | 25 May 2026 11:45:40 |
| Eccentricity: | 0.0002852 |
| inclination: | 97.4055° |
| perigee height: | 493 km |
| apogee height: | 497 km |
| right ascension of ascending node: | 226.2573° |
| argument of perigee: | 58.0263° |
| revolutions per day: | 15.23748476 |
| mean anomaly at epoch: | 302.1251° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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