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 26064.98700007 +.00000000 +00000-0 +34641-3 0 00009
2 31598 97.8862 255.9896 0000893 98.2893 261.8429 14.96498096 09
| Epoch (UTC): | 05 March 2026 23:41:16 |
| Eccentricity: | 0.0000893 |
| inclination: | 97.8862° |
| perigee height: | 577 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 255.9896° |
| argument of perigee: | 98.2893° |
| revolutions per day: | 14.96498096 |
| mean anomaly at epoch: | 261.8429° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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