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 55263U 26143.23572736 +.00000000 +00000-0 +00000-0 0 00005
2 55263 0.0036 320.7234 0000178 81.6333 307.1771 1.00272469 00
| Epoch (UTC): | 23 May 2026 05:39:26 |
| Eccentricity: | 0.0000178 |
| inclination: | 0.0036° |
| perigee height: | 35786 km |
| apogee height: | 35787 km |
| right ascension of ascending node: | 320.7234° |
| argument of perigee: | 81.6333° |
| revolutions per day: | 1.00272469 |
| mean anomaly at epoch: | 307.1771° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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