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 67824U 26145.57201102 +.00000000 +00000-0 +37675-3 0 00007
2 67824 43.0028 192.7402 0001428 272.4969 87.5719 15.27586569 06
| Epoch (UTC): | 25 May 2026 13:43:41 |
| Eccentricity: | 0.0001428 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 192.7402° |
| argument of perigee: | 272.4969° |
| revolutions per day: | 15.27586569 |
| mean anomaly at epoch: | 87.5719° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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