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 60319U 26145.45634488 +.00000000 +00000-0 +37942-4 0 00001
2 60319 53.1607 300.4902 0000959 88.9339 271.1772 15.30199314 07
| Epoch (UTC): | 25 May 2026 10:57:08 |
| Eccentricity: | 0.0000959 |
| inclination: | 53.1607° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 300.4902° |
| argument of perigee: | 88.9339° |
| revolutions per day: | 15.30199314 |
| mean anomaly at epoch: | 271.1772° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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