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 67975U 26145.50240127 +.00000000 +00000-0 +50406-3 0 00004
2 67975 97.2837 155.5653 0000894 64.3380 295.7955 15.33458206 06
| Epoch (UTC): | 25 May 2026 12:03:27 |
| Eccentricity: | 0.0000894 |
| inclination: | 97.2837° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 155.5653° |
| argument of perigee: | 64.3380° |
| revolutions per day: | 15.33458206 |
| mean anomaly at epoch: | 295.7955° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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