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 67565U 26145.42907278 +.00000000 +00000-0 +46248-3 0 00006
2 67565 97.2853 205.7394 0000185 233.8860 126.2366 15.33454232 07
| Epoch (UTC): | 25 May 2026 10:17:51 |
| Eccentricity: | 0.0000185 |
| inclination: | 97.2853° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 205.7394° |
| argument of perigee: | 233.8860° |
| revolutions per day: | 15.33454232 |
| mean anomaly at epoch: | 126.2366° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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