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 63227U 26145.64076634 +.00000000 +00000-0 +45160-3 0 00006
2 63227 97.3971 65.1010 0006298 130.8445 229.3384 16.07508646 05
| Epoch (UTC): | 25 May 2026 15:22:42 |
| Eccentricity: | 0.0006298 |
| inclination: | 97.3971° |
| perigee height: | 250 km |
| apogee height: | 258 km |
| right ascension of ascending node: | 65.1010° |
| argument of perigee: | 130.8445° |
| revolutions per day: | 16.07508646 |
| mean anomaly at epoch: | 229.3384° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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