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 47267U 26145.57454236 +.00000000 +00000-0 +11377-2 0 00004
2 47267 87.8960 355.1533 0001999 78.9591 281.1762 13.12441606 03
| Epoch (UTC): | 25 May 2026 13:47:20 |
| Eccentricity: | 0.0001999 |
| inclination: | 87.8960° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.1533° |
| argument of perigee: | 78.9591° |
| revolutions per day: | 13.12441606 |
| mean anomaly at epoch: | 281.1762° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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