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 26040.84757579 +.00000000 +00000-0 +33376-3 0 00008
2 31598 97.8858 231.6616 0000845 81.9279 278.2038 14.96310948 06
| Epoch (UTC): | 09 February 2026 20:20:30 |
| Eccentricity: | 0.0000845 |
| inclination: | 97.8858° |
| perigee height: | 578 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 231.6616° |
| argument of perigee: | 81.9279° |
| revolutions per day: | 14.96310948 |
| mean anomaly at epoch: | 278.2038° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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