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 26044.54413587 +.00000000 +00000-0 +13261-3 0 00007
2 03598 34.9919 91.6035 0046697 359.6564 0.4092 14.57545362 03
| Epoch (UTC): | 13 February 2026 13:03:33 |
| Eccentricity: | 0.0046697 |
| inclination: | 34.9919° |
| perigee height: | 668 km |
| apogee height: | 734 km |
| right ascension of ascending node: | 91.6035° |
| argument of perigee: | 359.6564° |
| revolutions per day: | 14.57545362 |
| mean anomaly at epoch: | 0.4092° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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