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 47841U 26145.52866404 +.00000000 +00000-0 +46240-4 0 00000
2 47841 53.1610 241.6756 0001663 85.9234 274.1958 15.31706038 00
| Epoch (UTC): | 25 May 2026 12:41:16 |
| Eccentricity: | 0.0001663 |
| inclination: | 53.1610° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 241.6756° |
| argument of perigee: | 85.9234° |
| revolutions per day: | 15.31706038 |
| mean anomaly at epoch: | 274.1958° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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