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 47733U 26145.58357014 +.00000000 +00000-0 +30951-5 0 00001
2 47733 53.1577 219.0539 0001421 85.3913 274.7250 15.31701641 06
| Epoch (UTC): | 25 May 2026 14:00:20 |
| Eccentricity: | 0.0001421 |
| inclination: | 53.1577° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 219.0539° |
| argument of perigee: | 85.3913° |
| revolutions per day: | 15.31701641 |
| mean anomaly at epoch: | 274.7250° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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