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 54127U 26145.42272142 +.00000000 +00000-0 +16236-3 0 00005
2 54127 87.9161 309.5010 0001702 90.4594 269.6733 13.19726060 03
| Epoch (UTC): | 25 May 2026 10:08:43 |
| Eccentricity: | 0.0001702 |
| inclination: | 87.9161° |
| perigee height: | 1184 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5010° |
| argument of perigee: | 90.4594° |
| revolutions per day: | 13.19726060 |
| mean anomaly at epoch: | 269.6733° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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