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 67163U 26145.31145894 +.00000000 +00000-0 +43734-3 0 00003
2 67163 43.0000 237.9806 0001344 248.9122 111.1586 15.27592197 08
| Epoch (UTC): | 25 May 2026 07:28:30 |
| Eccentricity: | 0.0001344 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 237.9806° |
| argument of perigee: | 248.9122° |
| revolutions per day: | 15.27592197 |
| mean anomaly at epoch: | 111.1586° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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