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 47750U 26145.59243242 +.00000000 +00000-0 +30020-4 0 00004
2 47750 53.1593 195.8539 0001223 85.4952 274.6189 15.31697923 05
| Epoch (UTC): | 25 May 2026 14:13:06 |
| Eccentricity: | 0.0001223 |
| inclination: | 53.1593° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 195.8539° |
| argument of perigee: | 85.4952° |
| revolutions per day: | 15.31697923 |
| mean anomaly at epoch: | 274.6189° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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