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 55785U 26145.33878152 +.00000000 +00000-0 +10250-3 0 00009
2 55785 69.9998 11.3527 0002136 275.0130 85.0785 14.98334890 03
| Epoch (UTC): | 25 May 2026 08:07:50 |
| Eccentricity: | 0.0002136 |
| inclination: | 69.9998° |
| perigee height: | 571 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 11.3527° |
| argument of perigee: | 275.0130° |
| revolutions per day: | 14.98334890 |
| mean anomaly at epoch: | 85.0785° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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