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 67533U 26145.64149797 +.00000000 +00000-0 +76271-3 0 00008
2 67533 97.2884 32.6356 0002196 95.3068 264.8425 15.33453921 05
| Epoch (UTC): | 25 May 2026 15:23:45 |
| Eccentricity: | 0.0002196 |
| inclination: | 97.2884° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 32.6356° |
| argument of perigee: | 95.3068° |
| revolutions per day: | 15.33453921 |
| mean anomaly at epoch: | 264.8425° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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