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 26067.37582066 +.00000000 +00000-0 +87550-4 0 00007
2 18215 82.5145 174.4952 0020707 59.9813 3.1285 14.85635080 06
| Epoch (UTC): | 08 March 2026 09:01:10 |
| Eccentricity: | 0.0020707 |
| inclination: | 82.5145° |
| perigee height: | 597 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 174.4952° |
| argument of perigee: | 59.9813° |
| revolutions per day: | 14.85635080 |
| mean anomaly at epoch: | 3.1285° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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