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 12677U 26053.22464623 +.00000000 +00000-0 +00000-0 0 00001
2 12677 8.2277 304.9483 0012329 331.4925 217.6692 0.99548566 01
| Epoch (UTC): | 22 February 2026 05:23:29 |
| Eccentricity: | 0.0012329 |
| inclination: | 8.2277° |
| perigee height: | 35938 km |
| apogee height: | 36043 km |
| right ascension of ascending node: | 304.9483° |
| argument of perigee: | 331.4925° |
| revolutions per day: | 0.99548566 |
| mean anomaly at epoch: | 217.6692° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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