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 26037.63767685 +.00000000 +00000-0 +50228-3 0 00005
2 31598 97.8856 228.4278 0001000 74.2128 285.9203 14.96289658 06
| Epoch (UTC): | 06 February 2026 15:18:15 |
| Eccentricity: | 0.0001000 |
| inclination: | 97.8856° |
| perigee height: | 578 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 228.4278° |
| argument of perigee: | 74.2128° |
| revolutions per day: | 14.96289658 |
| mean anomaly at epoch: | 285.9203° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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