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 26065.25445578 +.00000000 +00000-0 +33880-3 0 00003
2 31598 97.8863 256.2591 0000920 98.8639 261.2686 14.96500257 03
| Epoch (UTC): | 06 March 2026 06:06:24 |
| Eccentricity: | 0.0000920 |
| inclination: | 97.8863° |
| perigee height: | 577 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 256.2591° |
| argument of perigee: | 98.8639° |
| revolutions per day: | 14.96500257 |
| mean anomaly at epoch: | 261.2686° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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