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 67304U 26145.38046294 +.00000000 +00000-0 +40616-4 0 00008
2 67304 97.8885 329.3129 0001302 90.6370 269.4993 14.82150396 08
| Epoch (UTC): | 25 May 2026 09:07:51 |
| Eccentricity: | 0.0001302 |
| inclination: | 97.8885° |
| perigee height: | 622 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 329.3129° |
| argument of perigee: | 90.6370° |
| revolutions per day: | 14.82150396 |
| mean anomaly at epoch: | 269.4993° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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