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 53180U 26145.27485030 +.00000000 +00000-0 -71174-4 0 00002
2 53180 53.2137 140.1845 0001058 69.9807 290.1299 15.08846614 01
| Epoch (UTC): | 25 May 2026 06:35:47 |
| Eccentricity: | 0.0001058 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 140.1845° |
| argument of perigee: | 69.9807° |
| revolutions per day: | 15.08846614 |
| mean anomaly at epoch: | 290.1299° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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