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 48224U 26145.36902095 +.00000000 +00000-0 -33479-3 0 00005
2 48224 87.8946 294.2588 0001151 104.4684 255.6574 13.14501934 02
| Epoch (UTC): | 25 May 2026 08:51:23 |
| Eccentricity: | 0.0001151 |
| inclination: | 87.8946° |
| perigee height: | 1205 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2588° |
| argument of perigee: | 104.4684° |
| revolutions per day: | 13.14501934 |
| mean anomaly at epoch: | 255.6574° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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