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 67768U 26144.96596669 +.00000000 +00000-0 -12273-4 0 00000
2 67768 51.8972 230.8234 0000331 94.6944 265.4056 14.79936072 09
| Epoch (UTC): | 24 May 2026 23:10:59 |
| Eccentricity: | 0.0000331 |
| inclination: | 51.8972° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 230.8234° |
| argument of perigee: | 94.6944° |
| revolutions per day: | 14.79936072 |
| mean anomaly at epoch: | 265.4056° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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