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 15506U 26042.15700832 +.00000000 +00000-0 +79863-4 0 00007
2 15506 82.9180 107.3722 0035705 210.7600 167.6592 13.76504741 09
| Epoch (UTC): | 11 February 2026 03:46:05 |
| Eccentricity: | 0.0035705 |
| inclination: | 82.9180° |
| perigee height: | 950 km |
| apogee height: | 1003 km |
| right ascension of ascending node: | 107.3722° |
| argument of perigee: | 210.7600° |
| revolutions per day: | 13.76504741 |
| mean anomaly at epoch: | 167.6592° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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