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 26071.13836424 +.00000000 +00000-0 +35466-3 0 00003
2 31598 97.8879 262.1896 0001468 98.0922 262.0465 14.96556565 06
| Epoch (UTC): | 12 March 2026 03:19:14 |
| Eccentricity: | 0.0001468 |
| inclination: | 97.8879° |
| perigee height: | 577 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 262.1896° |
| argument of perigee: | 98.0922° |
| revolutions per day: | 14.96556565 |
| mean anomaly at epoch: | 262.0465° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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