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 62663U 26145.46370880 +.00000000 +00000-0 +29019-3 0 00004
2 62663 97.4028 227.9240 0004033 52.2836 307.8769 15.30004694 09
| Epoch (UTC): | 25 May 2026 11:07:44 |
| Eccentricity: | 0.0004033 |
| inclination: | 97.4028° |
| perigee height: | 473 km |
| apogee height: | 479 km |
| right ascension of ascending node: | 227.9240° |
| argument of perigee: | 52.2836° |
| revolutions per day: | 15.30004694 |
| mean anomaly at epoch: | 307.8769° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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