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 32060U 26145.57698168 +.00000000 +00000-0 +23188-3 0 00007
2 32060 97.3924 265.6500 0003968 120.4963 239.6667 15.24631020 05
| Epoch (UTC): | 25 May 2026 13:50:51 |
| Eccentricity: | 0.0003968 |
| inclination: | 97.3924° |
| perigee height: | 489 km |
| apogee height: | 495 km |
| right ascension of ascending node: | 265.6500° |
| argument of perigee: | 120.4963° |
| revolutions per day: | 15.24631020 |
| mean anomaly at epoch: | 239.6667° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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