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 67396U 26145.46817172 +.00000000 +00000-0 +21479-3 0 00004
2 67396 97.4523 144.8618 0008370 62.3824 297.8259 15.18920841 09
| Epoch (UTC): | 25 May 2026 11:14:10 |
| Eccentricity: | 0.0008370 |
| inclination: | 97.4523° |
| perigee height: | 503 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 144.8618° |
| argument of perigee: | 62.3824° |
| revolutions per day: | 15.18920841 |
| mean anomaly at epoch: | 297.8259° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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