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 67973U 26144.99123809 +.00000000 +00000-0 +44929-3 0 00004
2 67973 97.2824 155.0344 0002969 103.5186 256.6388 15.33456546 08
| Epoch (UTC): | 24 May 2026 23:47:22 |
| Eccentricity: | 0.0002969 |
| inclination: | 97.2824° |
| perigee height: | 463 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 155.0344° |
| argument of perigee: | 103.5186° |
| revolutions per day: | 15.33456546 |
| mean anomaly at epoch: | 256.6388° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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