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 67751U 26145.42641691 +.00000000 +00000-0 +11492-3 0 00000
2 67751 97.5051 273.3016 0009994 185.5357 174.5765 15.11986308 09
| Epoch (UTC): | 25 May 2026 10:14:02 |
| Eccentricity: | 0.0009994 |
| inclination: | 97.5051° |
| perigee height: | 523 km |
| apogee height: | 537 km |
| right ascension of ascending node: | 273.3016° |
| argument of perigee: | 185.5357° |
| revolutions per day: | 15.11986308 |
| mean anomaly at epoch: | 174.5765° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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