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 60305U 26145.34382705 +.00000000 +00000-0 +45279-5 0 00009
2 60305 53.1575 128.3344 0000907 82.3886 277.7235 15.69706783 03
| Epoch (UTC): | 25 May 2026 08:15:06 |
| Eccentricity: | 0.0000907 |
| inclination: | 53.1575° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 128.3344° |
| argument of perigee: | 82.3886° |
| revolutions per day: | 15.69706783 |
| mean anomaly at epoch: | 277.7235° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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