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 67776U 26145.60746014 +.00000000 +00000-0 +31108-3 0 00008
2 67776 51.8984 228.0722 0000440 171.1601 188.9369 14.79915264 00
| Epoch (UTC): | 25 May 2026 14:34:44 |
| Eccentricity: | 0.0000440 |
| inclination: | 51.8984° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 228.0722° |
| argument of perigee: | 171.1601° |
| revolutions per day: | 14.79915264 |
| mean anomaly at epoch: | 188.9369° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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