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 53996U 26145.52048677 +.00000000 +00000-0 +37596-4 0 00006
2 53996 53.2123 229.0529 0000984 87.8516 272.2588 15.08836454 03
| Epoch (UTC): | 25 May 2026 12:29:30 |
| Eccentricity: | 0.0000984 |
| inclination: | 53.2123° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 229.0529° |
| argument of perigee: | 87.8516° |
| revolutions per day: | 15.08836454 |
| mean anomaly at epoch: | 272.2588° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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