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 26016.93742529 +.00000000 +00000-0 +94436-4 0 00004
2 03598 34.9911 248.3038 0046132 135.9019 224.5367 14.57489749 03
| Epoch (UTC): | 16 January 2026 22:29:53 |
| Eccentricity: | 0.0046132 |
| inclination: | 34.9911° |
| perigee height: | 669 km |
| apogee height: | 734 km |
| right ascension of ascending node: | 248.3038° |
| argument of perigee: | 135.9019° |
| revolutions per day: | 14.57489749 |
| mean anomaly at epoch: | 224.5367° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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