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 13553U 26069.17613208 +.00000000 +00000-0 +58749-4 0 00008
2 13553 82.5694 140.9446 0018981 301.8277 87.9960 14.86666845 09
| Epoch (UTC): | 10 March 2026 04:13:37 |
| Eccentricity: | 0.0018981 |
| inclination: | 82.5694° |
| perigee height: | 595 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 140.9446° |
| argument of perigee: | 301.8277° |
| revolutions per day: | 14.86666845 |
| mean anomaly at epoch: | 87.9960° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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