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 13272U 26088.15276808 +.00000000 +00000-0 +70654-4 0 00005
2 13272 82.5134 2.7108 0016740 321.1219 38.8792 14.87192275 08
| Epoch (UTC): | 29 March 2026 03:39:59 |
| Eccentricity: | 0.0016740 |
| inclination: | 82.5134° |
| perigee height: | 595 km |
| apogee height: | 618 km |
| right ascension of ascending node: | 2.7108° |
| argument of perigee: | 321.1219° |
| revolutions per day: | 14.87192275 |
| mean anomaly at epoch: | 38.8792° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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