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 47824U 26145.29968904 +.00000000 +00000-0 +60340-4 0 00000
2 47824 53.1608 261.9429 0001350 84.1850 275.9304 15.30190582 02
| Epoch (UTC): | 25 May 2026 07:11:33 |
| Eccentricity: | 0.0001350 |
| inclination: | 53.1608° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 261.9429° |
| argument of perigee: | 84.1850° |
| revolutions per day: | 15.30190582 |
| mean anomaly at epoch: | 275.9304° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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