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 60392U 26145.64433875 +.00000000 +00000-0 +11639-3 0 00004
2 60392 88.9689 282.2591 0018705 95.9723 264.3561 13.51009469 00
| Epoch (UTC): | 25 May 2026 15:27:50 |
| Eccentricity: | 0.0018705 |
| inclination: | 88.9689° |
| perigee height: | 1055 km |
| apogee height: | 1082 km |
| right ascension of ascending node: | 282.2591° |
| argument of perigee: | 95.9723° |
| revolutions per day: | 13.51009469 |
| mean anomaly at epoch: | 264.3561° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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