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 53163U 26145.47728840 +.00000000 +00000-0 +35564-4 0 00006
2 53163 53.2120 179.5498 0001259 71.7829 288.3300 15.08836695 02
| Epoch (UTC): | 25 May 2026 11:27:17 |
| Eccentricity: | 0.0001259 |
| inclination: | 53.2120° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 179.5498° |
| argument of perigee: | 71.7829° |
| revolutions per day: | 15.08836695 |
| mean anomaly at epoch: | 288.3300° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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