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 47157U 26145.57747777 +.00000000 +00000-0 +23768-2 0 00004
2 47157 53.1572 298.3727 0001887 287.0787 73.0009 15.34645303 03
| Epoch (UTC): | 25 May 2026 13:51:34 |
| Eccentricity: | 0.0001887 |
| inclination: | 53.1572° |
| perigee height: | 461 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 298.3727° |
| argument of perigee: | 287.0787° |
| revolutions per day: | 15.34645303 |
| mean anomaly at epoch: | 73.0009° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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