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 18215U 26069.81143767 +.00000000 +00000-0 +70382-4 0 00004
2 18215 82.5145 172.2044 0020601 52.3679 69.0745 14.85637864 08
| Epoch (UTC): | 10 March 2026 19:28:28 |
| Eccentricity: | 0.0020601 |
| inclination: | 82.5145° |
| perigee height: | 597 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 172.2044° |
| argument of perigee: | 52.3679° |
| revolutions per day: | 14.85637864 |
| mean anomaly at epoch: | 69.0745° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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