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 60182U 26145.56912831 +.00000000 +00000-0 +17779-3 0 00007
2 60182 97.9231 243.0611 0001624 96.6735 263.4661 14.79475255 03
| Epoch (UTC): | 25 May 2026 13:39:32 |
| Eccentricity: | 0.0001624 |
| inclination: | 97.9231° |
| perigee height: | 630 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 243.0611° |
| argument of perigee: | 96.6735° |
| revolutions per day: | 14.79475255 |
| mean anomaly at epoch: | 263.4661° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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