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 47293U 26145.27637146 +.00000000 +00000-0 +65106-3 0 00003
2 47293 87.8960 355.1985 0001681 81.7838 278.3482 13.12441584 09
| Epoch (UTC): | 25 May 2026 06:37:58 |
| Eccentricity: | 0.0001681 |
| inclination: | 87.8960° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.1985° |
| argument of perigee: | 81.7838° |
| revolutions per day: | 13.12441584 |
| mean anomaly at epoch: | 278.3482° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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