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 26069.53368355 +.00000000 +00000-0 +39761-3 0 00009
2 31598 97.8874 260.5720 0001331 99.5351 260.6021 14.96543052 09
| Epoch (UTC): | 10 March 2026 12:48:30 |
| Eccentricity: | 0.0001331 |
| inclination: | 97.8874° |
| perigee height: | 577 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 260.5720° |
| argument of perigee: | 99.5351° |
| revolutions per day: | 14.96543052 |
| mean anomaly at epoch: | 260.6021° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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