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 67976U 26145.44529760 +.00000000 +00000-0 +71333-3 0 00003
2 67976 97.2855 155.4901 0001184 1.3399 358.7846 15.33451155 01
| Epoch (UTC): | 25 May 2026 10:41:13 |
| Eccentricity: | 0.0001184 |
| inclination: | 97.2855° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 155.4901° |
| argument of perigee: | 1.3399° |
| revolutions per day: | 15.33451155 |
| mean anomaly at epoch: | 358.7846° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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