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 67205U 26144.96496294 +.00000000 +00000-0 +34753-3 0 00004
2 67205 70.0018 341.9927 0002658 264.5190 95.5666 14.98339873 03
| Epoch (UTC): | 24 May 2026 23:09:32 |
| Eccentricity: | 0.0002658 |
| inclination: | 70.0018° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 341.9927° |
| argument of perigee: | 264.5190° |
| revolutions per day: | 14.98339873 |
| mean anomaly at epoch: | 95.5666° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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