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 53831U 26145.47542759 +.00000000 +00000-0 -17422-4 0 00005
2 53831 53.2142 319.3998 0001344 87.5113 272.6033 15.08839598 07
| Epoch (UTC): | 25 May 2026 11:24:36 |
| Eccentricity: | 0.0001344 |
| inclination: | 53.2142° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 319.3998° |
| argument of perigee: | 87.5113° |
| revolutions per day: | 15.08839598 |
| mean anomaly at epoch: | 272.6033° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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