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 27560U 26155.32026205 +.00000000 +00000-0 +12811-3 0 00008
2 27560 98.4415 11.8166 0039378 57.6173 30.3864 14.61792894 00
| Epoch (UTC): | 04 June 2026 07:41:10 |
| Eccentricity: | 0.0039378 |
| inclination: | 98.4415° |
| perigee height: | 660 km |
| apogee height: | 715 km |
| right ascension of ascending node: | 11.8166° |
| argument of perigee: | 57.6173° |
| revolutions per day: | 14.61792894 |
| mean anomaly at epoch: | 30.3864° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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