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 12472U 26106.78614763 +.00000000 +00000-0 +00000-0 0 00006
2 12472 9.4692 316.0782 0003853 345.4789 87.7129 1.00205445 09
| Epoch (UTC): | 16 April 2026 18:52:03 |
| Eccentricity: | 0.0003853 |
| inclination: | 9.4692° |
| perigee height: | 35789 km |
| apogee height: | 35821 km |
| right ascension of ascending node: | 316.0782° |
| argument of perigee: | 345.4789° |
| revolutions per day: | 1.00205445 |
| mean anomaly at epoch: | 87.7129° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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