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 26156.85362747 +.00000000 +00000-0 +50579-4 0 00002
2 15399 82.9448 94.9410 0033795 0.6512 53.0176 13.76456722 07
| Epoch (UTC): | 05 June 2026 20:29:13 |
| Eccentricity: | 0.0033795 |
| inclination: | 82.9448° |
| perigee height: | 952 km |
| apogee height: | 1001 km |
| right ascension of ascending node: | 94.9410° |
| argument of perigee: | 0.6512° |
| revolutions per day: | 13.76456722 |
| mean anomaly at epoch: | 53.0176° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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