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 53855U 26145.18655031 +.00000000 +00000-0 +81313-4 0 00006
2 53855 53.2140 310.4564 0001265 86.9552 273.1585 15.08840122 07
| Epoch (UTC): | 25 May 2026 04:28:37 |
| Eccentricity: | 0.0001265 |
| inclination: | 53.2140° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 310.4564° |
| argument of perigee: | 86.9552° |
| revolutions per day: | 15.08840122 |
| mean anomaly at epoch: | 273.1585° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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