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 67623U 26145.46613326 +.00000000 +00000-0 +64006-3 0 00005
2 67623 42.9997 66.3605 0000618 250.3170 109.7615 15.27588988 05
| Epoch (UTC): | 25 May 2026 11:11:13 |
| Eccentricity: | 0.0000618 |
| inclination: | 42.9997° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 66.3605° |
| argument of perigee: | 250.3170° |
| revolutions per day: | 15.27588988 |
| mean anomaly at epoch: | 109.7615° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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