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 60545U 26145.16781855 +.00000000 +00000-0 +15923-3 0 00005
2 60545 97.6820 220.8538 0005963 153.2526 206.9005 14.96432739 09
| Epoch (UTC): | 25 May 2026 04:01:39 |
| Eccentricity: | 0.0005963 |
| inclination: | 97.6820° |
| perigee height: | 574 km |
| apogee height: | 582 km |
| right ascension of ascending node: | 220.8538° |
| argument of perigee: | 153.2526° |
| revolutions per day: | 14.96432739 |
| mean anomaly at epoch: | 206.9005° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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