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 60595U 26145.46787964 +.00000000 +00000-0 +18227-3 0 00000
2 60595 53.1610 310.5992 0001142 72.2772 287.8353 15.30203305 05
| Epoch (UTC): | 25 May 2026 11:13:44 |
| Eccentricity: | 0.0001142 |
| inclination: | 53.1610° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 310.5992° |
| argument of perigee: | 72.2772° |
| revolutions per day: | 15.30203305 |
| mean anomaly at epoch: | 287.8353° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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