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 67582U 26145.61668779 +.00000000 +00000-0 +31028-3 0 00006
2 67582 97.2850 205.9447 0000625 93.9873 266.1441 15.33441945 07
| Epoch (UTC): | 25 May 2026 14:48:01 |
| Eccentricity: | 0.0000625 |
| inclination: | 97.2850° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 205.9447° |
| argument of perigee: | 93.9873° |
| revolutions per day: | 15.33441945 |
| mean anomaly at epoch: | 266.1441° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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