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 60518U 26145.14927856 +.00000000 +00000-0 +41356-3 0 00005
2 60518 97.3780 229.9250 0004099 39.4953 320.6592 15.41717753 08
| Epoch (UTC): | 25 May 2026 03:34:57 |
| Eccentricity: | 0.0004099 |
| inclination: | 97.3780° |
| perigee height: | 438 km |
| apogee height: | 444 km |
| right ascension of ascending node: | 229.9250° |
| argument of perigee: | 39.4953° |
| revolutions per day: | 15.41717753 |
| mean anomaly at epoch: | 320.6592° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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