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 67319U 26144.71221977 +.00000000 +00000-0 +55981-3 0 00003
2 67319 43.0022 256.1028 0001453 265.8660 94.2026 15.27599306 09
| Epoch (UTC): | 24 May 2026 17:05:35 |
| Eccentricity: | 0.0001453 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 256.1028° |
| argument of perigee: | 265.8660° |
| revolutions per day: | 15.27599306 |
| mean anomaly at epoch: | 94.2026° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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