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 39088U 26151.84854730 +.00000000 +00000-0 +58554-4 0 00006
2 39088 98.4255 331.6929 0010122 301.0642 58.9550 14.35235744 08
| Epoch (UTC): | 31 May 2026 20:21:54 |
| Eccentricity: | 0.0010122 |
| inclination: | 98.4255° |
| perigee height: | 767 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 331.6929° |
| argument of perigee: | 301.0642° |
| revolutions per day: | 14.35235744 |
| mean anomaly at epoch: | 58.9550° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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