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 41785U 26145.60824904 +.00000000 +00000-0 +11409-3 0 00007
2 41785 97.7759 155.3474 0008091 305.6601 54.3853 14.72255557 00
| Epoch (UTC): | 25 May 2026 14:35:52 |
| Eccentricity: | 0.0008091 |
| inclination: | 97.7759° |
| perigee height: | 648 km |
| apogee height: | 660 km |
| right ascension of ascending node: | 155.3474° |
| argument of perigee: | 305.6601° |
| revolutions per day: | 14.72255557 |
| mean anomaly at epoch: | 54.3853° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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