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 53272U 26145.42022770 +.00000000 +00000-0 +41525-4 0 00005
2 53272 53.2123 199.6633 0001333 61.7031 298.4095 15.08838061 09
| Epoch (UTC): | 25 May 2026 10:05:07 |
| Eccentricity: | 0.0001333 |
| inclination: | 53.2123° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 199.6633° |
| argument of perigee: | 61.7031° |
| revolutions per day: | 15.08838061 |
| mean anomaly at epoch: | 298.4095° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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