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 53902U 26145.35672189 +.00000000 +00000-0 -65134-4 0 00005
2 53902 53.2157 289.7009 0001358 90.8265 269.2883 15.08840341 08
| Epoch (UTC): | 25 May 2026 08:33:40 |
| Eccentricity: | 0.0001358 |
| inclination: | 53.2157° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 289.7009° |
| argument of perigee: | 90.8265° |
| revolutions per day: | 15.08840341 |
| mean anomaly at epoch: | 269.2883° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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