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 60519U 26145.13280851 +.00000000 +00000-0 +39309-3 0 00007
2 60519 97.3744 230.5618 0004131 33.2655 326.8852 15.43992725 06
| Epoch (UTC): | 25 May 2026 03:11:14 |
| Eccentricity: | 0.0004131 |
| inclination: | 97.3744° |
| perigee height: | 432 km |
| apogee height: | 437 km |
| right ascension of ascending node: | 230.5618° |
| argument of perigee: | 33.2655° |
| revolutions per day: | 15.43992725 |
| mean anomaly at epoch: | 326.8852° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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