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 67128U 26145.54707176 +.00000000 +00000-0 +30366-3 0 00003
2 67128 42.9973 94.6762 0000403 281.4518 78.6288 15.27584196 07
| Epoch (UTC): | 25 May 2026 13:07:47 |
| Eccentricity: | 0.0000403 |
| inclination: | 42.9973° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 94.6762° |
| argument of perigee: | 281.4518° |
| revolutions per day: | 15.27584196 |
| mean anomaly at epoch: | 78.6288° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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