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 54144U 26145.37375119 +.00000000 +00000-0 -75558-4 0 00000
2 54144 87.9158 309.5116 0001688 93.5883 266.5443 13.19727449 09
| Epoch (UTC): | 25 May 2026 08:58:12 |
| Eccentricity: | 0.0001688 |
| inclination: | 87.9158° |
| perigee height: | 1184 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5116° |
| argument of perigee: | 93.5883° |
| revolutions per day: | 13.19727449 |
| mean anomaly at epoch: | 266.5443° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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