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 55285U 26145.46178529 +.00000000 +00000-0 +11012-3 0 00006
2 55285 69.9985 170.8072 0003559 268.4064 91.6687 14.98324737 05
| Epoch (UTC): | 25 May 2026 11:04:58 |
| Eccentricity: | 0.0003559 |
| inclination: | 69.9985° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 170.8072° |
| argument of perigee: | 268.4064° |
| revolutions per day: | 14.98324737 |
| mean anomaly at epoch: | 91.6687° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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