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 48053U 26145.46801753 +.00000000 +00000-0 +22694-3 0 00001
2 48053 87.8942 324.7454 0001761 98.0813 262.0516 13.13469351 01
| Epoch (UTC): | 25 May 2026 11:13:56 |
| Eccentricity: | 0.0001761 |
| inclination: | 87.8942° |
| perigee height: | 1208 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7454° |
| argument of perigee: | 98.0813° |
| revolutions per day: | 13.13469351 |
| mean anomaly at epoch: | 262.0516° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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