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 47790U 26145.46705163 +.00000000 +00000-0 +36357-4 0 00008
2 47790 53.1575 219.5937 0001542 85.9420 274.1757 15.31702909 01
| Epoch (UTC): | 25 May 2026 11:12:33 |
| Eccentricity: | 0.0001542 |
| inclination: | 53.1575° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 219.5937° |
| argument of perigee: | 85.9420° |
| revolutions per day: | 15.31702909 |
| mean anomaly at epoch: | 274.1757° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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