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 03597U 26088.23749654 +.00000000 +00000-0 +83557-4 0 00003
2 03597 34.9924 156.0797 0005703 348.5775 11.4785 14.47318850 03
| Epoch (UTC): | 29 March 2026 05:41:59 |
| Eccentricity: | 0.0005703 |
| inclination: | 34.9924° |
| perigee height: | 730 km |
| apogee height: | 738 km |
| right ascension of ascending node: | 156.0797° |
| argument of perigee: | 348.5775° |
| revolutions per day: | 14.47318850 |
| mean anomaly at epoch: | 11.4785° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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