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 39269U 26145.49192957 +.00000000 +00000-0 +18791-3 0 00005
2 39269 80.9912 170.1633 0418053 266.7825 88.5495 14.90653610 02
| Epoch (UTC): | 25 May 2026 11:48:22 |
| Eccentricity: | 0.0418053 |
| inclination: | 80.9912° |
| perigee height: | 304 km |
| apogee height: | 887 km |
| right ascension of ascending node: | 170.1633° |
| argument of perigee: | 266.7825° |
| revolutions per day: | 14.90653610 |
| mean anomaly at epoch: | 88.5495° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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