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 67727U 26145.61877194 +.00000000 +00000-0 +11187-2 0 00003
2 67727 97.2847 199.1067 0001166 75.4113 284.7259 15.33478389 04
| Epoch (UTC): | 25 May 2026 14:51:01 |
| Eccentricity: | 0.0001166 |
| inclination: | 97.2847° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 199.1067° |
| argument of perigee: | 75.4113° |
| revolutions per day: | 15.33478389 |
| mean anomaly at epoch: | 284.7259° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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