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 60521U 26145.51804302 +.00000000 +00000-0 +95879-3 0 00009
2 60521 97.3775 239.8700 0002474 262.2228 97.8756 15.75437850 01
| Epoch (UTC): | 25 May 2026 12:25:58 |
| Eccentricity: | 0.0002474 |
| inclination: | 97.3775° |
| perigee height: | 342 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 239.8700° |
| argument of perigee: | 262.2228° |
| revolutions per day: | 15.75437850 |
| mean anomaly at epoch: | 97.8756° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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