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 61267U 26018.77551847 +.00000000 +00000-0 +70934-3 0 00002
2 61267 89.1570 300.9227 0052635 349.4758 10.5328 14.24027996 01
| Epoch (UTC): | 18 January 2026 18:36:44 |
| Eccentricity: | 0.0052635 |
| inclination: | 89.1570° |
| perigee height: | 774 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 300.9227° |
| argument of perigee: | 349.4758° |
| revolutions per day: | 14.24027996 |
| mean anomaly at epoch: | 10.5328° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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