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 55239U 26144.82603763 +.00000000 +00000-0 +00000-0 0 00009
2 55239 0.0131 246.4257 0000502 307.9398 119.4031 1.00272251 06
| Epoch (UTC): | 24 May 2026 19:49:29 |
| Eccentricity: | 0.0000502 |
| inclination: | 0.0131° |
| perigee height: | 35784 km |
| apogee height: | 35789 km |
| right ascension of ascending node: | 246.4257° |
| argument of perigee: | 307.9398° |
| revolutions per day: | 1.00272251 |
| mean anomaly at epoch: | 119.4031° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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