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 67684U 26145.12814611 +.00000000 +00000-0 +11132-2 0 00006
2 67684 51.6259 46.3144 0013096 121.3622 238.8658 15.68546210 07
| Epoch (UTC): | 25 May 2026 03:04:31 |
| Eccentricity: | 0.0013096 |
| inclination: | 51.6259° |
| perigee height: | 354 km |
| apogee height: | 372 km |
| right ascension of ascending node: | 46.3144° |
| argument of perigee: | 121.3622° |
| revolutions per day: | 15.68546210 |
| mean anomaly at epoch: | 238.8658° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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