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 26067.92898727 +.00000000 +00000-0 +46490-3 0 00008
2 31598 97.8870 258.9546 0001168 100.5461 259.5892 14.96528628 00
| Epoch (UTC): | 08 March 2026 22:17:44 |
| Eccentricity: | 0.0001168 |
| inclination: | 97.8870° |
| perigee height: | 577 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 258.9546° |
| argument of perigee: | 100.5461° |
| revolutions per day: | 14.96528628 |
| mean anomaly at epoch: | 259.5892° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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