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 60238U 26145.49397053 +.00000000 +00000-0 +46155-3 0 00004
2 60238 61.9883 286.3541 0041462 126.7249 233.7665 15.11282455 09
| Epoch (UTC): | 25 May 2026 11:51:19 |
| Eccentricity: | 0.0041462 |
| inclination: | 61.9883° |
| perigee height: | 504 km |
| apogee height: | 561 km |
| right ascension of ascending node: | 286.3541° |
| argument of perigee: | 126.7249° |
| revolutions per day: | 15.11282455 |
| mean anomaly at epoch: | 233.7665° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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