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 67912U 26145.46192628 +.00000000 +00000-0 +45046-3 0 00006
2 67912 43.0044 171.6678 0001797 272.0169 88.0477 15.27584771 00
| Epoch (UTC): | 25 May 2026 11:05:10 |
| Eccentricity: | 0.0001797 |
| inclination: | 43.0044° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 171.6678° |
| argument of perigee: | 272.0169° |
| revolutions per day: | 15.27584771 |
| mean anomaly at epoch: | 88.0477° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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