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 26065.27797814 +.00000000 +00000-0 +70758-4 0 00005
2 13553 82.5700 144.5903 0019204 315.6120 104.2493 14.86662436 00
| Epoch (UTC): | 06 March 2026 06:40:17 |
| Eccentricity: | 0.0019204 |
| inclination: | 82.5700° |
| perigee height: | 595 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 144.5903° |
| argument of perigee: | 315.6120° |
| revolutions per day: | 14.86662436 |
| mean anomaly at epoch: | 104.2493° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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