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 15399U 26088.23516530 +.00000000 +00000-0 +11239-3 0 00008
2 15399 82.9460 145.8845 0033585 187.4254 237.1589 13.76450949 01
| Epoch (UTC): | 29 March 2026 05:38:38 |
| Eccentricity: | 0.0033585 |
| inclination: | 82.9460° |
| perigee height: | 952 km |
| apogee height: | 1001 km |
| right ascension of ascending node: | 145.8845° |
| argument of perigee: | 187.4254° |
| revolutions per day: | 13.76450949 |
| mean anomaly at epoch: | 237.1589° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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