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 67539U 26145.42669078 +.00000000 +00000-0 +41521-3 0 00009
2 67539 97.2866 32.4698 0000461 209.9979 150.1237 15.33450855 06
| Epoch (UTC): | 25 May 2026 10:14:26 |
| Eccentricity: | 0.0000461 |
| inclination: | 97.2866° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 32.4698° |
| argument of perigee: | 209.9979° |
| revolutions per day: | 15.33450855 |
| mean anomaly at epoch: | 150.1237° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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