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 06392U 26100.03530372 +.00000000 +00000-0 +10475-3 0 00005
2 06392 81.2413 354.2776 0055520 32.8030 327.6565 14.08106271 02
| Epoch (UTC): | 10 April 2026 00:50:50 |
| Eccentricity: | 0.0055520 |
| inclination: | 81.2413° |
| perigee height: | 826 km |
| apogee height: | 906 km |
| right ascension of ascending node: | 354.2776° |
| argument of perigee: | 32.8030° |
| revolutions per day: | 14.08106271 |
| mean anomaly at epoch: | 327.6565° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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