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 31598U 26064.18463071 +.00000000 +00000-0 +39136-3 0 00002
2 31598 97.8861 255.1810 0000847 95.4148 264.7169 14.96491406 08
| Epoch (UTC): | 05 March 2026 04:25:52 |
| Eccentricity: | 0.0000847 |
| inclination: | 97.8861° |
| perigee height: | 577 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 255.1810° |
| argument of perigee: | 95.4148° |
| revolutions per day: | 14.96491406 |
| mean anomaly at epoch: | 264.7169° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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