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 62528U 26145.45479247 +.00000000 +00000-0 +55084-3 0 00001
2 62528 42.9993 145.9353 0000911 318.8508 41.2275 15.27596640 01
| Epoch (UTC): | 25 May 2026 10:54:54 |
| Eccentricity: | 0.0000911 |
| inclination: | 42.9993° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 145.9353° |
| argument of perigee: | 318.8508° |
| revolutions per day: | 15.27596640 |
| mean anomaly at epoch: | 41.2275° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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