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 47625U 26145.18068038 +.00000000 +00000-0 +79641-3 0 00009
2 47625 53.0474 56.0306 0007285 90.9549 269.2296 15.54927305 04
| Epoch (UTC): | 25 May 2026 04:20:10 |
| Eccentricity: | 0.0007285 |
| inclination: | 53.0474° |
| perigee height: | 397 km |
| apogee height: | 407 km |
| right ascension of ascending node: | 56.0306° |
| argument of perigee: | 90.9549° |
| revolutions per day: | 15.54927305 |
| mean anomaly at epoch: | 269.2296° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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