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 53794U 26145.43128729 +.00000000 +00000-0 +27426-4 0 00000
2 53794 53.2137 289.4594 0001196 86.1976 273.9152 15.08838650 09
| Epoch (UTC): | 25 May 2026 10:21:03 |
| Eccentricity: | 0.0001196 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 289.4594° |
| argument of perigee: | 86.1976° |
| revolutions per day: | 15.08838650 |
| mean anomaly at epoch: | 273.9152° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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