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 60750U 26145.64268991 +.00000000 +00000-0 +51773-3 0 00000
2 60750 97.6683 281.6512 0004612 339.2755 20.8295 15.25269219 09
| Epoch (UTC): | 25 May 2026 15:25:28 |
| Eccentricity: | 0.0004612 |
| inclination: | 97.6683° |
| perigee height: | 487 km |
| apogee height: | 493 km |
| right ascension of ascending node: | 281.6512° |
| argument of perigee: | 339.2755° |
| revolutions per day: | 15.25269219 |
| mean anomaly at epoch: | 20.8295° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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