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 67140U 26145.15676583 +.00000000 +00000-0 -84622-3 0 00006
2 67140 51.9014 99.9869 0000604 113.0949 247.0077 14.79925611 09
| Epoch (UTC): | 25 May 2026 03:45:44 |
| Eccentricity: | 0.0000604 |
| inclination: | 51.9014° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 99.9869° |
| argument of perigee: | 113.0949° |
| revolutions per day: | 14.79925611 |
| mean anomaly at epoch: | 247.0077° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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