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 68943U 26145.38136676 +.00000000 +00000-0 +36351-3 0 00002
2 68943 51.8762 177.6656 0006953 63.7475 296.4224 15.34164839 07
| Epoch (UTC): | 25 May 2026 09:09:10 |
| Eccentricity: | 0.0006953 |
| inclination: | 51.8762° |
| perigee height: | 459 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 177.6656° |
| argument of perigee: | 63.7475° |
| revolutions per day: | 15.34164839 |
| mean anomaly at epoch: | 296.4224° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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