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 63822U 26145.14074981 +.00000000 +00000-0 +88316-3 0 00005
2 63822 42.9963 97.5708 0001007 219.9550 140.1228 15.27604772 00
| Epoch (UTC): | 25 May 2026 03:22:40 |
| Eccentricity: | 0.0001007 |
| inclination: | 42.9963° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 97.5708° |
| argument of perigee: | 219.9550° |
| revolutions per day: | 15.27604772 |
| mean anomaly at epoch: | 140.1228° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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