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 48052U 26145.49340782 +.00000000 +00000-0 +76198-3 0 00001
2 48052 87.8951 324.7383 0001811 96.1814 263.9522 13.13468441 03
| Epoch (UTC): | 25 May 2026 11:50:30 |
| Eccentricity: | 0.0001811 |
| inclination: | 87.8951° |
| perigee height: | 1208 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7383° |
| argument of perigee: | 96.1814° |
| revolutions per day: | 13.13468441 |
| mean anomaly at epoch: | 263.9522° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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