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 26068.30805044 +.00000000 +00000-0 +61137-4 0 00008
2 13553 82.5696 141.7565 0019009 304.9287 121.8021 14.86665887 00
| Epoch (UTC): | 09 March 2026 07:23:35 |
| Eccentricity: | 0.0019009 |
| inclination: | 82.5696° |
| perigee height: | 595 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 141.7565° |
| argument of perigee: | 304.9287° |
| revolutions per day: | 14.86665887 |
| mean anomaly at epoch: | 121.8021° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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