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 26075.22978700 +.00000000 +00000-0 +10050-3 0 00006
2 40069 98.5031 54.3023 0005005 317.1891 42.8897 14.21431827 05
| Epoch (UTC): | 16 March 2026 05:30:53 |
| Eccentricity: | 0.0005005 |
| inclination: | 98.5031° |
| perigee height: | 817 km |
| apogee height: | 824 km |
| right ascension of ascending node: | 54.3023° |
| argument of perigee: | 317.1891° |
| revolutions per day: | 14.21431827 |
| mean anomaly at epoch: | 42.8897° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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