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 26101.27456360 +.00000000 +00000-0 +27446-3 0 00001
2 40069 98.5075 79.4019 0004759 223.9060 136.1740 14.21443680 07
| Epoch (UTC): | 11 April 2026 06:35:22 |
| Eccentricity: | 0.0004759 |
| inclination: | 98.5075° |
| perigee height: | 817 km |
| apogee height: | 824 km |
| right ascension of ascending node: | 79.4019° |
| argument of perigee: | 223.9060° |
| revolutions per day: | 14.21443680 |
| mean anomaly at epoch: | 136.1740° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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