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 40069U 26088.18180686 +.00000000 +00000-0 +17657-3 0 00003
2 40069 98.5054 66.7825 0004541 271.4017 88.6641 14.21437477 05
| Epoch (UTC): | 29 March 2026 04:21:48 |
| Eccentricity: | 0.0004541 |
| inclination: | 98.5054° |
| perigee height: | 817 km |
| apogee height: | 824 km |
| right ascension of ascending node: | 66.7825° |
| argument of perigee: | 271.4017° |
| revolutions per day: | 14.21437477 |
| mean anomaly at epoch: | 88.6641° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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