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 26044.92674816 +.00000000 +00000-0 +31995-3 0 00008
2 31598 97.8858 235.7716 0001082 94.1423 265.9922 14.96341594 09
| Epoch (UTC): | 13 February 2026 22:14:31 |
| Eccentricity: | 0.0001082 |
| inclination: | 97.8858° |
| perigee height: | 577 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 235.7716° |
| argument of perigee: | 94.1423° |
| revolutions per day: | 14.96341594 |
| mean anomaly at epoch: | 265.9922° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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