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 47903U 26145.66668980 +.00000000 +00000-0 +85279-3 0 00007
2 47903 53.1537 231.2434 0006218 331.1444 10.2546 15.81054927 05
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0006218 |
| inclination: | 53.1537° |
| perigee height: | 323 km |
| apogee height: | 332 km |
| right ascension of ascending node: | 231.2434° |
| argument of perigee: | 331.1444° |
| revolutions per day: | 15.81054927 |
| mean anomaly at epoch: | 10.2546° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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