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 26137.87777883 +.00000000 +00000-0 -80842-4 0 00003
2 40069 98.5095 114.6927 0006768 117.9633 242.2231 14.21451811 08
| Epoch (UTC): | 17 May 2026 21:04:00 |
| Eccentricity: | 0.0006768 |
| inclination: | 98.5095° |
| perigee height: | 816 km |
| apogee height: | 825 km |
| right ascension of ascending node: | 114.6927° |
| argument of perigee: | 117.9633° |
| revolutions per day: | 14.21451811 |
| mean anomaly at epoch: | 242.2231° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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