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 03598U 26100.50902744 +.00000000 +00000-0 +89642-4 0 00001
2 03598 34.9907 133.9140 0046080 96.6695 263.9247 14.57613711 08
| Epoch (UTC): | 10 April 2026 12:12:59 |
| Eccentricity: | 0.0046080 |
| inclination: | 34.9907° |
| perigee height: | 668 km |
| apogee height: | 734 km |
| right ascension of ascending node: | 133.9140° |
| argument of perigee: | 96.6695° |
| revolutions per day: | 14.57613711 |
| mean anomaly at epoch: | 263.9247° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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