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 67595U 26145.42073117 +.00000000 +00000-0 +64474-3 0 00006
2 67595 97.2853 210.5471 0000423 108.8051 251.3237 15.33452766 05
| Epoch (UTC): | 25 May 2026 10:05:51 |
| Eccentricity: | 0.0000423 |
| inclination: | 97.2853° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 210.5471° |
| argument of perigee: | 108.8051° |
| revolutions per day: | 15.33452766 |
| mean anomaly at epoch: | 251.3237° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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