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 68384U 26145.39827848 +.00000000 +00000-0 +74090-3 0 00002
2 68384 97.2823 287.9952 0001250 89.2073 270.9313 15.33435920 01
| Epoch (UTC): | 25 May 2026 09:33:31 |
| Eccentricity: | 0.0001250 |
| inclination: | 97.2823° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 287.9952° |
| argument of perigee: | 89.2073° |
| revolutions per day: | 15.33435920 |
| mean anomaly at epoch: | 270.9313° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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