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 26106.23752112 +.00000000 +00000-0 +87242-4 0 00004
2 31598 97.8878 297.5788 0001331 85.6548 274.4825 14.96801393 01
| Epoch (UTC): | 16 April 2026 05:42:01 |
| Eccentricity: | 0.0001331 |
| inclination: | 97.8878° |
| perigee height: | 576 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 297.5788° |
| argument of perigee: | 85.6548° |
| revolutions per day: | 14.96801393 |
| mean anomaly at epoch: | 274.4825° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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