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 67078U 26145.39305556 +.00000000 +00000-0 +29069-3 0 00004
2 67078 70.0014 181.1858 0003993 268.3590 91.7112 14.98337687 08
| Epoch (UTC): | 25 May 2026 09:26:00 |
| Eccentricity: | 0.0003993 |
| inclination: | 70.0014° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 181.1858° |
| argument of perigee: | 268.3590° |
| revolutions per day: | 14.98337687 |
| mean anomaly at epoch: | 91.7112° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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