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 47919U 26145.11951480 +.00000000 +00000-0 +20748-3 0 00004
2 47919 53.1591 285.4838 0001205 101.2295 258.8842 15.31709030 08
| Epoch (UTC): | 25 May 2026 02:52:06 |
| Eccentricity: | 0.0001205 |
| inclination: | 53.1591° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 285.4838° |
| argument of perigee: | 101.2295° |
| revolutions per day: | 15.31709030 |
| mean anomaly at epoch: | 258.8842° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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