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 26066.77903528 +.00000000 +00000-0 +86194-4 0 00003
2 18215 82.5145 175.0565 0020726 61.8207 51.4846 14.85634089 00
| Epoch (UTC): | 07 March 2026 18:41:48 |
| Eccentricity: | 0.0020726 |
| inclination: | 82.5145° |
| perigee height: | 597 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 175.0565° |
| argument of perigee: | 61.8207° |
| revolutions per day: | 14.85634089 |
| mean anomaly at epoch: | 51.4846° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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