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 40047U 26088.18991810 +.00000000 +00000-0 +37203-4 0 00008
2 40047 97.8806 321.7256 0568230 145.5048 218.4387 13.61953299 03
| Epoch (UTC): | 29 March 2026 04:33:28 |
| Eccentricity: | 0.0568230 |
| inclination: | 97.8806° |
| perigee height: | 608 km |
| apogee height: | 1449 km |
| right ascension of ascending node: | 321.7256° |
| argument of perigee: | 145.5048° |
| revolutions per day: | 13.61953299 |
| mean anomaly at epoch: | 218.4387° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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