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 47536U 26145.59828699 +.00000000 +00000-0 -15588-3 0 00003
2 47536 63.4022 200.1954 0174080 0.5700 359.5493 13.45445088 07
| Epoch (UTC): | 25 May 2026 14:21:31 |
| Eccentricity: | 0.0174080 |
| inclination: | 63.4022° |
| perigee height: | 959 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 200.1954° |
| argument of perigee: | 0.5700° |
| revolutions per day: | 13.45445088 |
| mean anomaly at epoch: | 359.5493° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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