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 67685U 26144.97483317 +.00000000 +00000-0 +61449-3 0 00001
2 67685 51.6289 50.5589 0013488 113.7790 246.4618 15.58858192 02
| Epoch (UTC): | 24 May 2026 23:23:45 |
| Eccentricity: | 0.0013488 |
| inclination: | 51.6289° |
| perigee height: | 382 km |
| apogee height: | 400 km |
| right ascension of ascending node: | 50.5589° |
| argument of perigee: | 113.7790° |
| revolutions per day: | 15.58858192 |
| mean anomaly at epoch: | 246.4618° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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