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 60038U 26145.26551681 +.00000000 +00000-0 +39640-5 0 00009
2 60038 53.1610 249.1073 0000604 71.9703 288.1380 15.69710871 03
| Epoch (UTC): | 25 May 2026 06:22:20 |
| Eccentricity: | 0.0000604 |
| inclination: | 53.1610° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 249.1073° |
| argument of perigee: | 71.9703° |
| revolutions per day: | 15.69710871 |
| mean anomaly at epoch: | 288.1380° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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