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 47945U 26145.48441144 +.00000000 +00000-0 +33677-3 0 00009
2 47945 97.3911 50.1807 0010331 145.0250 215.1676 15.39769241 02
| Epoch (UTC): | 25 May 2026 11:37:33 |
| Eccentricity: | 0.0010331 |
| inclination: | 97.3911° |
| perigee height: | 440 km |
| apogee height: | 454 km |
| right ascension of ascending node: | 50.1807° |
| argument of perigee: | 145.0250° |
| revolutions per day: | 15.39769241 |
| mean anomaly at epoch: | 215.1676° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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