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 67059U 26145.60276889 +.00000000 +00000-0 +89369-4 0 00003
2 67059 50.0026 106.7820 0000864 354.7541 5.3322 13.29327483 00
| Epoch (UTC): | 25 May 2026 14:27:59 |
| Eccentricity: | 0.0000864 |
| inclination: | 50.0026° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 106.7820° |
| argument of perigee: | 354.7541° |
| revolutions per day: | 13.29327483 |
| mean anomaly at epoch: | 5.3322° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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