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 63371U 26145.47826388 +.00000000 +00000-0 +30709-3 0 00009
2 63371 53.1595 55.9618 0001693 99.8263 260.2929 15.30206398 07
| Epoch (UTC): | 25 May 2026 11:28:41 |
| Eccentricity: | 0.0001693 |
| inclination: | 53.1595° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 55.9618° |
| argument of perigee: | 99.8263° |
| revolutions per day: | 15.30206398 |
| mean anomaly at epoch: | 260.2929° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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