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 69179U 26142.86980617 +.00000000 +00000-0 +14133-3 0 00000
2 69179 44.9083 325.1175 0286327 260.0946 96.7520 15.61899702 08
| Epoch (UTC): | 22 May 2026 20:52:31 |
| Eccentricity: | 0.0286327 |
| inclination: | 44.9083° |
| perigee height: | 189 km |
| apogee height: | 576 km |
| right ascension of ascending node: | 325.1175° |
| argument of perigee: | 260.0946° |
| revolutions per day: | 15.61899702 |
| mean anomaly at epoch: | 96.7520° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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