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 67967U 26145.46705419 +.00000000 +00000-0 +46784-3 0 00004
2 67967 97.2859 155.4604 0001065 111.7349 248.4007 15.33457911 04
| Epoch (UTC): | 25 May 2026 11:12:33 |
| Eccentricity: | 0.0001065 |
| inclination: | 97.2859° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 155.4604° |
| argument of perigee: | 111.7349° |
| revolutions per day: | 15.33457911 |
| mean anomaly at epoch: | 248.4007° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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