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 60508U 26145.52685683 +.00000000 +00000-0 +70372-3 0 00005
2 60508 97.3723 237.6862 0001366 325.3658 34.7514 15.66678842 01
| Epoch (UTC): | 25 May 2026 12:38:40 |
| Eccentricity: | 0.0001366 |
| inclination: | 97.3723° |
| perigee height: | 367 km |
| apogee height: | 369 km |
| right ascension of ascending node: | 237.6862° |
| argument of perigee: | 325.3658° |
| revolutions per day: | 15.66678842 |
| mean anomaly at epoch: | 34.7514° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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