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 67682U 26145.13548508 +.00000000 +00000-0 +41334-3 0 00002
2 67682 96.6266 211.8047 0021242 196.4411 163.6143 15.24873932 04
| Epoch (UTC): | 25 May 2026 03:15:05 |
| Eccentricity: | 0.0021242 |
| inclination: | 96.6266° |
| perigee height: | 477 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 211.8047° |
| argument of perigee: | 196.4411° |
| revolutions per day: | 15.24873932 |
| mean anomaly at epoch: | 163.6143° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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