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 48445U 26145.47183527 +.00000000 +00000-0 +36587-4 0 00006
2 48445 53.1595 180.9953 0001302 88.8707 271.2443 15.31698806 04
| Epoch (UTC): | 25 May 2026 11:19:26 |
| Eccentricity: | 0.0001302 |
| inclination: | 53.1595° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 180.9953° |
| argument of perigee: | 88.8707° |
| revolutions per day: | 15.31698806 |
| mean anomaly at epoch: | 271.2443° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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