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 69177U 26142.82127166 +.00000000 +00000-0 +29927-4 0 00004
2 69177 44.9091 325.6494 0027124 267.7288 92.0478 15.01794608 09
| Epoch (UTC): | 22 May 2026 19:42:37 |
| Eccentricity: | 0.0027124 |
| inclination: | 44.9091° |
| perigee height: | 543 km |
| apogee height: | 580 km |
| right ascension of ascending node: | 325.6494° |
| argument of perigee: | 267.7288° |
| revolutions per day: | 15.01794608 |
| mean anomaly at epoch: | 92.0478° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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