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 60381U 26145.48393727 +.00000000 +00000-0 +13574-3 0 00005
2 60381 88.9693 282.2230 0015916 89.2935 271.0040 13.51006927 08
| Epoch (UTC): | 25 May 2026 11:36:52 |
| Eccentricity: | 0.0015916 |
| inclination: | 88.9693° |
| perigee height: | 1057 km |
| apogee height: | 1080 km |
| right ascension of ascending node: | 282.2230° |
| argument of perigee: | 89.2935° |
| revolutions per day: | 13.51006927 |
| mean anomaly at epoch: | 271.0040° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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