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 47613U 26145.54840919 +.00000000 +00000-0 +00000-0 0 00002
2 47613 0.5443 87.8468 0002281 326.3826 204.8419 1.00269417 01
| Epoch (UTC): | 25 May 2026 13:09:42 |
| Eccentricity: | 0.0002281 |
| inclination: | 0.5443° |
| perigee height: | 35778 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 87.8468° |
| argument of perigee: | 326.3826° |
| revolutions per day: | 1.00269417 |
| mean anomaly at epoch: | 204.8419° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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