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 67436U 26145.46833660 +.00000000 +00000-0 +95701-4 0 00009
2 67436 50.0038 167.4478 0000897 282.9668 77.1104 13.29324436 03
| Epoch (UTC): | 25 May 2026 11:14:24 |
| Eccentricity: | 0.0000897 |
| inclination: | 50.0038° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 167.4478° |
| argument of perigee: | 282.9668° |
| revolutions per day: | 13.29324436 |
| mean anomaly at epoch: | 77.1104° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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