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 47235U 26058.19405615 +.00000000 +00000-0 +23073-3 0 00004
2 47235 28.9982 10.8844 0010635 257.2071 102.7339 15.01652363 02
| Epoch (UTC): | 27 February 2026 04:39:26 |
| Eccentricity: | 0.0010635 |
| inclination: | 28.9982° |
| perigee height: | 554 km |
| apogee height: | 569 km |
| right ascension of ascending node: | 10.8844° |
| argument of perigee: | 257.2071° |
| revolutions per day: | 15.01652363 |
| mean anomaly at epoch: | 102.7339° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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