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 60516U 26144.78038381 +.00000000 +00000-0 +33033-3 0 00001
2 60516 97.3784 228.2400 0003830 46.6204 313.5360 15.38848754 06
| Epoch (UTC): | 24 May 2026 18:43:45 |
| Eccentricity: | 0.0003830 |
| inclination: | 97.3784° |
| perigee height: | 447 km |
| apogee height: | 452 km |
| right ascension of ascending node: | 228.2400° |
| argument of perigee: | 46.6204° |
| revolutions per day: | 15.38848754 |
| mean anomaly at epoch: | 313.5360° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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