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 47731U 26145.41600978 +.00000000 +00000-0 +10559-2 0 00000
2 47731 53.1536 193.7813 0007764 350.8000 9.2871 15.61959451 02
| Epoch (UTC): | 25 May 2026 09:59:03 |
| Eccentricity: | 0.0007764 |
| inclination: | 53.1536° |
| perigee height: | 377 km |
| apogee height: | 387 km |
| right ascension of ascending node: | 193.7813° |
| argument of perigee: | 350.8000° |
| revolutions per day: | 15.61959451 |
| mean anomaly at epoch: | 9.2871° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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