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 63219U 26144.68749552 +.00000000 +00000-0 +45480-3 0 00001
2 63219 97.3903 40.6449 0002628 158.7421 201.3931 15.32970600 09
| Epoch (UTC): | 24 May 2026 16:29:59 |
| Eccentricity: | 0.0002628 |
| inclination: | 97.3903° |
| perigee height: | 465 km |
| apogee height: | 469 km |
| right ascension of ascending node: | 40.6449° |
| argument of perigee: | 158.7421° |
| revolutions per day: | 15.32970600 |
| mean anomaly at epoch: | 201.3931° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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