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 53999U 26145.52786087 +.00000000 +00000-0 +39611-4 0 00003
2 53999 53.2140 229.0977 0001577 77.8850 282.2319 15.08833871 04
| Epoch (UTC): | 25 May 2026 12:40:07 |
| Eccentricity: | 0.0001577 |
| inclination: | 53.2140° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 229.0977° |
| argument of perigee: | 77.8850° |
| revolutions per day: | 15.08833871 |
| mean anomaly at epoch: | 282.2319° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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