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 26159.13445940 +.00000000 +00000-0 +53626-4 0 00007
2 13272 82.5094 295.7230 0019236 82.4185 277.9216 14.87249969 05
| Epoch (UTC): | 08 June 2026 03:13:37 |
| Eccentricity: | 0.0019236 |
| inclination: | 82.5094° |
| perigee height: | 593 km |
| apogee height: | 620 km |
| right ascension of ascending node: | 295.7230° |
| argument of perigee: | 82.4185° |
| revolutions per day: | 14.87249969 |
| mean anomaly at epoch: | 277.9216° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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