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 60517U 26145.49951936 +.00000000 +00000-0 +40701-3 0 00001
2 60517 97.3694 229.0819 0004516 39.0425 321.1147 15.40188701 03
| Epoch (UTC): | 25 May 2026 11:59:18 |
| Eccentricity: | 0.0004516 |
| inclination: | 97.3694° |
| perigee height: | 442 km |
| apogee height: | 449 km |
| right ascension of ascending node: | 229.0819° |
| argument of perigee: | 39.0425° |
| revolutions per day: | 15.40188701 |
| mean anomaly at epoch: | 321.1147° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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