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 12668U 26073.27325965 +.00000000 +00000-0 +40140-3 0 00005
2 12668 83.1070 155.8905 0054795 128.4506 303.5539 14.03420270 04
| Epoch (UTC): | 14 March 2026 06:33:29 |
| Eccentricity: | 0.0054795 |
| inclination: | 83.1070° |
| perigee height: | 842 km |
| apogee height: | 922 km |
| right ascension of ascending node: | 155.8905° |
| argument of perigee: | 128.4506° |
| revolutions per day: | 14.03420270 |
| mean anomaly at epoch: | 303.5539° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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