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 60676U 26017.99368167 +.00000000 +00000-0 +11835-3 0 00004
2 60676 88.9452 288.7642 0069227 332.7758 26.9806 14.13895151 00
| Epoch (UTC): | 17 January 2026 23:50:54 |
| Eccentricity: | 0.0069227 |
| inclination: | 88.9452° |
| perigee height: | 796 km |
| apogee height: | 896 km |
| right ascension of ascending node: | 288.7642° |
| argument of perigee: | 332.7758° |
| revolutions per day: | 14.13895151 |
| mean anomaly at epoch: | 26.9806° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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