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 53053U 26145.39287243 +.00000000 +00000-0 -11149-3 0 00005
2 53053 97.4478 325.2584 0001336 77.0260 283.1116 15.05665432 00
| Epoch (UTC): | 25 May 2026 09:25:44 |
| Eccentricity: | 0.0001336 |
| inclination: | 97.4478° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 325.2584° |
| argument of perigee: | 77.0260° |
| revolutions per day: | 15.05665432 |
| mean anomaly at epoch: | 283.1116° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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