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 67681U 26145.14727023 +.00000000 +00000-0 +31651-3 0 00004
2 67681 96.6311 211.8391 0021343 199.7019 160.3399 15.24556644 03
| Epoch (UTC): | 25 May 2026 03:32:04 |
| Eccentricity: | 0.0021343 |
| inclination: | 96.6311° |
| perigee height: | 477 km |
| apogee height: | 507 km |
| right ascension of ascending node: | 211.8391° |
| argument of perigee: | 199.7019° |
| revolutions per day: | 15.24556644 |
| mean anomaly at epoch: | 160.3399° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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