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 40045U 26053.01953538 +.00000000 +00000-0 +55438-3 0 00004
2 40045 97.7117 221.3795 0040209 42.7974 317.6366 14.96592962 09
| Epoch (UTC): | 22 February 2026 00:28:07 |
| Eccentricity: | 0.0040209 |
| inclination: | 97.7117° |
| perigee height: | 549 km |
| apogee height: | 605 km |
| right ascension of ascending node: | 221.3795° |
| argument of perigee: | 42.7974° |
| revolutions per day: | 14.96592962 |
| mean anomaly at epoch: | 317.6366° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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