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 63349U 26145.62629957 +.00000000 +00000-0 +16167-3 0 00006
2 63349 97.6102 327.2605 0014135 233.8428 126.1495 15.11094220 04
| Epoch (UTC): | 25 May 2026 15:01:52 |
| Eccentricity: | 0.0014135 |
| inclination: | 97.6102° |
| perigee height: | 523 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 327.2605° |
| argument of perigee: | 233.8428° |
| revolutions per day: | 15.11094220 |
| mean anomaly at epoch: | 126.1495° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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