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 54089U 26145.57937527 +.00000000 +00000-0 -19317-4 0 00008
2 54089 53.2118 348.8214 0001407 88.8427 271.2726 15.08838284 01
| Epoch (UTC): | 25 May 2026 13:54:18 |
| Eccentricity: | 0.0001407 |
| inclination: | 53.2118° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 348.8214° |
| argument of perigee: | 88.8427° |
| revolutions per day: | 15.08838284 |
| mean anomaly at epoch: | 271.2726° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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