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 60060U 26145.49688841 +.00000000 +00000-0 +21656-4 0 00005
2 60060 53.1586 172.6551 0001133 74.9039 285.2104 15.69706716 09
| Epoch (UTC): | 25 May 2026 11:55:31 |
| Eccentricity: | 0.0001133 |
| inclination: | 53.1586° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 172.6551° |
| argument of perigee: | 74.9039° |
| revolutions per day: | 15.69706716 |
| mean anomaly at epoch: | 285.2104° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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