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 67142U 26145.58335647 +.00000000 +00000-0 +21662-2 0 00001
2 67142 51.9024 68.2111 0001772 98.4295 22.1440 14.80409209 06
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001772 |
| inclination: | 51.9024° |
| perigee height: | 627 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 68.2111° |
| argument of perigee: | 98.4295° |
| revolutions per day: | 14.80409209 |
| mean anomaly at epoch: | 22.1440° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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