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 55355U 26145.51620575 +.00000000 +00000-0 -18061-5 0 00007
2 55355 43.0022 229.4575 0001447 277.4963 82.5724 15.27577723 08
| Epoch (UTC): | 25 May 2026 12:23:20 |
| Eccentricity: | 0.0001447 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 229.4575° |
| argument of perigee: | 277.4963° |
| revolutions per day: | 15.27577723 |
| mean anomaly at epoch: | 82.5724° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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