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 67773U 26145.52917168 +.00000000 +00000-0 +47083-3 0 00005
2 67773 51.9059 238.3537 0000422 116.1678 243.9328 14.79965753 07
| Epoch (UTC): | 25 May 2026 12:42:00 |
| Eccentricity: | 0.0000422 |
| inclination: | 51.9059° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 238.3537° |
| argument of perigee: | 116.1678° |
| revolutions per day: | 14.79965753 |
| mean anomaly at epoch: | 243.9328° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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