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 26145.54322538 +.00000000 +00000-0 +25049-3 0 00002
2 31598 97.8862 337.2103 0001737 96.4939 263.6480 14.96974440 02
| Epoch (UTC): | 25 May 2026 13:02:14 |
| Eccentricity: | 0.0001737 |
| inclination: | 97.8862° |
| perigee height: | 575 km |
| apogee height: | 577 km |
| right ascension of ascending node: | 337.2103° |
| argument of perigee: | 96.4939° |
| revolutions per day: | 14.96974440 |
| mean anomaly at epoch: | 263.6480° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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