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 18153U 26069.82293154 +.00000000 +00000-0 +72230-4 0 00006
2 18153 82.5030 347.9636 0021067 14.1244 346.0556 14.85631015 01
| Epoch (UTC): | 10 March 2026 19:45:01 |
| Eccentricity: | 0.0021067 |
| inclination: | 82.5030° |
| perigee height: | 597 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 347.9636° |
| argument of perigee: | 14.1244° |
| revolutions per day: | 14.85631015 |
| mean anomaly at epoch: | 346.0556° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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