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 67029U 26145.39815961 +.00000000 +00000-0 +27838-3 0 00008
2 67029 70.0008 261.2181 0003675 269.7025 90.3713 14.98335826 06
| Epoch (UTC): | 25 May 2026 09:33:20 |
| Eccentricity: | 0.0003675 |
| inclination: | 70.0008° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 261.2181° |
| argument of perigee: | 269.7025° |
| revolutions per day: | 14.98335826 |
| mean anomaly at epoch: | 90.3713° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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