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 67624U 26145.18788034 +.00000000 +00000-0 +62516-3 0 00008
2 67624 43.0027 67.7087 0001192 267.5098 92.5617 15.27593142 07
| Epoch (UTC): | 25 May 2026 04:30:32 |
| Eccentricity: | 0.0001192 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 67.7087° |
| argument of perigee: | 267.5098° |
| revolutions per day: | 15.27593142 |
| mean anomaly at epoch: | 92.5617° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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