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 54652U 26145.32641883 +.00000000 +00000-0 +17741-3 0 00001
2 54652 87.9255 248.5181 0001830 101.5293 258.6046 13.21824759 05
| Epoch (UTC): | 25 May 2026 07:50:02 |
| Eccentricity: | 0.0001830 |
| inclination: | 87.9255° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.5181° |
| argument of perigee: | 101.5293° |
| revolutions per day: | 13.21824759 |
| mean anomaly at epoch: | 258.6046° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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