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 67767U 26145.51367109 +.00000000 +00000-0 +24220-3 0 00009
2 67767 51.8994 232.8274 0000424 100.7022 259.3987 14.76452651 05
| Epoch (UTC): | 25 May 2026 12:19:41 |
| Eccentricity: | 0.0000424 |
| inclination: | 51.8994° |
| perigee height: | 640 km |
| apogee height: | 641 km |
| right ascension of ascending node: | 232.8274° |
| argument of perigee: | 100.7022° |
| revolutions per day: | 14.76452651 |
| mean anomaly at epoch: | 259.3987° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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