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 60211U 26145.36404177 +.00000000 +00000-0 +45956-4 0 00006
2 60211 97.8212 153.2414 0001565 90.6642 269.4753 14.87574030 00
| Epoch (UTC): | 25 May 2026 08:44:13 |
| Eccentricity: | 0.0001565 |
| inclination: | 97.8212° |
| perigee height: | 604 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 153.2414° |
| argument of perigee: | 90.6642° |
| revolutions per day: | 14.87574030 |
| mean anomaly at epoch: | 269.4753° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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