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 45222U 26145.61622378 +.00000000 +00000-0 +17157-2 0 00004
2 45222 53.1545 359.4240 0002318 139.9131 220.2045 15.37566848 06
| Epoch (UTC): | 25 May 2026 14:47:21 |
| Eccentricity: | 0.0002318 |
| inclination: | 53.1545° |
| perigee height: | 452 km |
| apogee height: | 455 km |
| right ascension of ascending node: | 359.4240° |
| argument of perigee: | 139.9131° |
| revolutions per day: | 15.37566848 |
| mean anomaly at epoch: | 220.2045° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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