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 60497U 26145.21197941 +.00000000 +00000-0 +42373-3 0 00003
2 60497 97.3722 228.9058 0003160 26.6409 333.4999 15.41261056 00
| Epoch (UTC): | 25 May 2026 05:05:15 |
| Eccentricity: | 0.0003160 |
| inclination: | 97.3722° |
| perigee height: | 440 km |
| apogee height: | 445 km |
| right ascension of ascending node: | 228.9058° |
| argument of perigee: | 26.6409° |
| revolutions per day: | 15.41261056 |
| mean anomaly at epoch: | 333.4999° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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