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 68388U 26145.66473847 +.00000000 +00000-0 +47496-3 0 00002
2 68388 97.2860 288.2465 0001918 91.4982 268.6480 15.33452796 03
| Epoch (UTC): | 25 May 2026 15:57:13 |
| Eccentricity: | 0.0001918 |
| inclination: | 97.2860° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 288.2465° |
| argument of perigee: | 91.4982° |
| revolutions per day: | 15.33452796 |
| mean anomaly at epoch: | 268.6480° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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