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 21047U 26086.17336477 +.00000000 +00000-0 +00000-0 0 00007
2 21047 13.0332 355.2547 0004469 255.7995 316.0578 0.98284872 02
| Epoch (UTC): | 27 March 2026 04:09:38 |
| Eccentricity: | 0.0004469 |
| inclination: | 13.0332° |
| perigee height: | 36334 km |
| apogee height: | 36372 km |
| right ascension of ascending node: | 355.2547° |
| argument of perigee: | 255.7995° |
| revolutions per day: | 0.98284872 |
| mean anomaly at epoch: | 316.0578° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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