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 48063U 26145.47139456 +.00000000 +00000-0 +35520-3 0 00009
2 48063 87.8950 324.7443 0001793 88.9346 271.1988 13.13468864 05
| Epoch (UTC): | 25 May 2026 11:18:48 |
| Eccentricity: | 0.0001793 |
| inclination: | 87.8950° |
| perigee height: | 1208 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7443° |
| argument of perigee: | 88.9346° |
| revolutions per day: | 13.13468864 |
| mean anomaly at epoch: | 271.1988° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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