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 12930U 26150.52123816 +.00000000 +00000-0 +00000-0 0 00000
2 12930 5.6108 1.5690 1043588 44.0068 111.3672 1.00394881 04
| Epoch (UTC): | 30 May 2026 12:30:34 |
| Eccentricity: | 0.1043588 |
| inclination: | 5.6108° |
| perigee height: | 31355 km |
| apogee height: | 40149 km |
| right ascension of ascending node: | 1.5690° |
| argument of perigee: | 44.0068° |
| revolutions per day: | 1.00394881 |
| mean anomaly at epoch: | 111.3672° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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