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 60306U 26145.33892138 +.00000000 +00000-0 +35510-5 0 00002
2 60306 53.1586 128.3032 0000974 86.2301 273.8828 15.69708386 05
| Epoch (UTC): | 25 May 2026 08:08:02 |
| Eccentricity: | 0.0000974 |
| inclination: | 53.1586° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 128.3032° |
| argument of perigee: | 86.2301° |
| revolutions per day: | 15.69708386 |
| mean anomaly at epoch: | 273.8828° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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