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 60371U 26144.66250181 +.00000000 +00000-0 -16444-3 0 00009
2 60371 53.1614 316.4163 0000515 97.9314 262.1745 15.30225069 07
| Epoch (UTC): | 24 May 2026 15:54:00 |
| Eccentricity: | 0.0000515 |
| inclination: | 53.1614° |
| perigee height: | 475 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 316.4163° |
| argument of perigee: | 97.9314° |
| revolutions per day: | 15.30225069 |
| mean anomaly at epoch: | 262.1745° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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