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 40732U 26088.11705823 +.00000000 +00000-0 +00000-0 0 00000
2 40732 3.0002 71.5321 0001774 285.0188 241.3418 1.00273915 04
| Epoch (UTC): | 29 March 2026 02:48:33 |
| Eccentricity: | 0.0001774 |
| inclination: | 3.0002° |
| perigee height: | 35779 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 71.5321° |
| argument of perigee: | 285.0188° |
| revolutions per day: | 1.00273915 |
| mean anomaly at epoch: | 241.3418° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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