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 40752U 26109.97638931 +.00000000 +00000-0 +18127-2 0 00006
2 40752 102.2206 193.8172 0566133 210.7295 329.3853 11.37653188 00
| Epoch (UTC): | 19 April 2026 23:26:00 |
| Eccentricity: | 0.0566133 |
| inclination: | 102.2206° |
| perigee height: | 1500 km |
| apogee height: | 2445 km |
| right ascension of ascending node: | 193.8172° |
| argument of perigee: | 210.7295° |
| revolutions per day: | 11.37653188 |
| mean anomaly at epoch: | 329.3853° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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