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 60471U 26145.49826132 +.00000000 +00000-0 +31815-3 0 00005
2 60471 97.3796 227.4965 0000863 33.0277 327.1020 15.35488641 05
| Epoch (UTC): | 25 May 2026 11:57:29 |
| Eccentricity: | 0.0000863 |
| inclination: | 97.3796° |
| perigee height: | 459 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 227.4965° |
| argument of perigee: | 33.0277° |
| revolutions per day: | 15.35488641 |
| mean anomaly at epoch: | 327.1020° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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