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 67646U 26145.62672484 +.00000000 +00000-0 +22774-3 0 00004
2 67646 97.4592 219.5327 0013959 240.7090 119.2752 15.23122425 09
| Epoch (UTC): | 25 May 2026 15:02:29 |
| Eccentricity: | 0.0013959 |
| inclination: | 97.4592° |
| perigee height: | 487 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 219.5327° |
| argument of perigee: | 240.7090° |
| revolutions per day: | 15.23122425 |
| mean anomaly at epoch: | 119.2752° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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