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 53841U 26145.15620610 +.00000000 +00000-0 +13172-3 0 00000
2 53841 53.2125 310.9773 0001099 123.0727 237.0371 15.08850577 01
| Epoch (UTC): | 25 May 2026 03:44:56 |
| Eccentricity: | 0.0001099 |
| inclination: | 53.2125° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 310.9773° |
| argument of perigee: | 123.0727° |
| revolutions per day: | 15.08850577 |
| mean anomaly at epoch: | 237.0371° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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