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 67178U 26145.24479214 +.00000000 +00000-0 +59661-3 0 00003
2 67178 42.9982 238.3376 0000183 356.3986 3.6864 15.27606618 08
| Epoch (UTC): | 25 May 2026 05:52:30 |
| Eccentricity: | 0.0000183 |
| inclination: | 42.9982° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 238.3376° |
| argument of perigee: | 356.3986° |
| revolutions per day: | 15.27606618 |
| mean anomaly at epoch: | 3.6864° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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