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 26159.47085845 +.00000000 +00000-0 +52815-4 0 00007
2 13272 82.5094 295.4056 0019233 81.3860 278.9536 14.87250316 07
| Epoch (UTC): | 08 June 2026 11:18:02 |
| Eccentricity: | 0.0019233 |
| inclination: | 82.5094° |
| perigee height: | 593 km |
| apogee height: | 620 km |
| right ascension of ascending node: | 295.4056° |
| argument of perigee: | 81.3860° |
| revolutions per day: | 14.87250316 |
| mean anomaly at epoch: | 278.9536° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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