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 67954U 26145.28413462 +.00000000 +00000-0 +89064-3 0 00002
2 67954 43.0000 118.2714 0001403 271.9023 88.1668 15.27595898 02
| Epoch (UTC): | 25 May 2026 06:49:09 |
| Eccentricity: | 0.0001403 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 118.2714° |
| argument of perigee: | 271.9023° |
| revolutions per day: | 15.27595898 |
| mean anomaly at epoch: | 88.1668° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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