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 68368U 26145.15292647 +.00000000 +00000-0 +30325-3 0 00004
2 68368 82.2970 38.2444 0006950 173.4769 186.6592 15.84329112 06
| Epoch (UTC): | 25 May 2026 03:40:12 |
| Eccentricity: | 0.0006950 |
| inclination: | 82.2970° |
| perigee height: | 314 km |
| apogee height: | 323 km |
| right ascension of ascending node: | 38.2444° |
| argument of perigee: | 173.4769° |
| revolutions per day: | 15.84329112 |
| mean anomaly at epoch: | 186.6592° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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