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 47375U 26145.50849422 +.00000000 +00000-0 +63513-4 0 00003
2 47375 53.1612 65.2344 0001171 85.1993 274.9142 15.31709798 04
| Epoch (UTC): | 25 May 2026 12:12:13 |
| Eccentricity: | 0.0001171 |
| inclination: | 53.1612° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 65.2344° |
| argument of perigee: | 85.1993° |
| revolutions per day: | 15.31709798 |
| mean anomaly at epoch: | 274.9142° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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