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 69041U 26145.58335647 +.00000000 +00000-0 -25422-1 0 00009
2 69041 97.2849 0.3765 0001403 90.4755 266.5366 15.69506047 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001403 |
| inclination: | 97.2849° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 0.3765° |
| argument of perigee: | 90.4755° |
| revolutions per day: | 15.69506047 |
| mean anomaly at epoch: | 266.5366° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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