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 26161.55405918 +.00000000 +00000-0 +41056-4 0 00003
2 18215 82.5117 85.8691 0020973 104.6898 72.4076 14.85710268 05
| Epoch (UTC): | 10 June 2026 13:17:50 |
| Eccentricity: | 0.0020973 |
| inclination: | 82.5117° |
| perigee height: | 597 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 85.8691° |
| argument of perigee: | 104.6898° |
| revolutions per day: | 14.85710268 |
| mean anomaly at epoch: | 72.4076° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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