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 40012U 26066.38650689 +.00000000 +00000-0 +55159-3 0 00003
2 40012 97.7724 221.0127 0046265 45.3615 315.1359 14.87618735 04
| Epoch (UTC): | 07 March 2026 09:16:34 |
| Eccentricity: | 0.0046265 |
| inclination: | 97.7724° |
| perigee height: | 573 km |
| apogee height: | 638 km |
| right ascension of ascending node: | 221.0127° |
| argument of perigee: | 45.3615° |
| revolutions per day: | 14.87618735 |
| mean anomaly at epoch: | 315.1359° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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