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 53389U 26145.28953845 +.00000000 +00000-0 +25504-3 0 00002
2 53389 53.2124 140.2463 0001576 79.0437 281.0732 15.08911337 07
| Epoch (UTC): | 25 May 2026 06:56:56 |
| Eccentricity: | 0.0001576 |
| inclination: | 53.2124° |
| perigee height: | 538 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 140.2463° |
| argument of perigee: | 79.0437° |
| revolutions per day: | 15.08911337 |
| mean anomaly at epoch: | 281.0732° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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