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 63222U 26145.14729642 +.00000000 +00000-0 +22369-3 0 00006
2 63222 97.4003 38.9046 0003893 185.7829 174.3364 15.24044997 06
| Epoch (UTC): | 25 May 2026 03:32:06 |
| Eccentricity: | 0.0003893 |
| inclination: | 97.4003° |
| perigee height: | 491 km |
| apogee height: | 496 km |
| right ascension of ascending node: | 38.9046° |
| argument of perigee: | 185.7829° |
| revolutions per day: | 15.24044997 |
| mean anomaly at epoch: | 174.3364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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