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 68596U 26145.58335647 +.00000000 +00000-0 -13647+0 0 00007
2 68596 51.8806 288.2297 0009472 310.7053 143.9109 15.11547030 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0009472 |
| inclination: | 51.8806° |
| perigee height: | 525 km |
| apogee height: | 538 km |
| right ascension of ascending node: | 288.2297° |
| argument of perigee: | 310.7053° |
| revolutions per day: | 15.11547030 |
| mean anomaly at epoch: | 143.9109° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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