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 54128U 26145.32923562 +.00000000 +00000-0 +27920-3 0 00006
2 54128 87.9175 278.9930 0002297 106.0847 254.0540 13.20771866 04
| Epoch (UTC): | 25 May 2026 07:54:05 |
| Eccentricity: | 0.0002297 |
| inclination: | 87.9175° |
| perigee height: | 1180 km |
| apogee height: | 1184 km |
| right ascension of ascending node: | 278.9930° |
| argument of perigee: | 106.0847° |
| revolutions per day: | 13.20771866 |
| mean anomaly at epoch: | 254.0540° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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