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 67933U 26145.30468956 +.00000000 +00000-0 +68856-3 0 00006
2 67933 43.0028 118.4397 0001805 266.8132 93.2513 15.27607908 00
| Epoch (UTC): | 25 May 2026 07:18:45 |
| Eccentricity: | 0.0001805 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 118.4397° |
| argument of perigee: | 266.8132° |
| revolutions per day: | 15.27607908 |
| mean anomaly at epoch: | 93.2513° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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