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 60540U 26145.10110192 +.00000000 +00000-0 +15420-3 0 00006
2 60540 97.6899 221.4098 0004635 131.1051 229.0571 14.96430722 05
| Epoch (UTC): | 25 May 2026 02:25:35 |
| Eccentricity: | 0.0004635 |
| inclination: | 97.6899° |
| perigee height: | 575 km |
| apogee height: | 581 km |
| right ascension of ascending node: | 221.4098° |
| argument of perigee: | 131.1051° |
| revolutions per day: | 14.96430722 |
| mean anomaly at epoch: | 229.0571° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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