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 60993U 26145.30837208 +.00000000 +00000-0 +10486-4 0 00002
2 60993 53.1597 263.9115 0000879 110.3904 249.7209 15.69711159 06
| Epoch (UTC): | 25 May 2026 07:24:03 |
| Eccentricity: | 0.0000879 |
| inclination: | 53.1597° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 263.9115° |
| argument of perigee: | 110.3904° |
| revolutions per day: | 15.69711159 |
| mean anomaly at epoch: | 249.7209° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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