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 53861U 26145.42208729 +.00000000 +00000-0 -15606-4 0 00001
2 53861 53.2127 299.8150 0001254 88.5471 271.5664 15.08839277 05
| Epoch (UTC): | 25 May 2026 10:07:48 |
| Eccentricity: | 0.0001254 |
| inclination: | 53.2127° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 299.8150° |
| argument of perigee: | 88.5471° |
| revolutions per day: | 15.08839277 |
| mean anomaly at epoch: | 271.5664° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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