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 67599U 26145.60290149 +.00000000 +00000-0 +66394-3 0 00009
2 67599 97.2850 210.7585 0000789 325.1727 34.9464 15.33458301 01
| Epoch (UTC): | 25 May 2026 14:28:10 |
| Eccentricity: | 0.0000789 |
| inclination: | 97.2850° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 210.7585° |
| argument of perigee: | 325.1727° |
| revolutions per day: | 15.33458301 |
| mean anomaly at epoch: | 34.9464° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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