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 48653U 26145.19483755 +.00000000 +00000-0 +36570-4 0 00004
2 48653 53.1594 118.0418 0001249 87.4609 272.6535 15.31702425 08
| Epoch (UTC): | 25 May 2026 04:40:33 |
| Eccentricity: | 0.0001249 |
| inclination: | 53.1594° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 118.0418° |
| argument of perigee: | 87.4609° |
| revolutions per day: | 15.31702425 |
| mean anomaly at epoch: | 272.6535° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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