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 55506U 26144.86596685 +.00000000 +00000-0 +00000-0 0 00004
2 55506 0.0853 208.0654 0000488 332.4270 179.5040 1.00271879 06
| Epoch (UTC): | 24 May 2026 20:46:59 |
| Eccentricity: | 0.0000488 |
| inclination: | 0.0853° |
| perigee height: | 35785 km |
| apogee height: | 35789 km |
| right ascension of ascending node: | 208.0654° |
| argument of perigee: | 332.4270° |
| revolutions per day: | 1.00271879 |
| mean anomaly at epoch: | 179.5040° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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