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 06324U 26073.61857344 +.00000000 +00000-0 +10178-3 0 00004
2 06324 74.0763 305.0847 0008800 335.4898 24.5840 14.45283604 07
| Epoch (UTC): | 14 March 2026 14:50:44 |
| Eccentricity: | 0.0008800 |
| inclination: | 74.0763° |
| perigee height: | 735 km |
| apogee height: | 747 km |
| right ascension of ascending node: | 305.0847° |
| argument of perigee: | 335.4898° |
| revolutions per day: | 14.45283604 |
| mean anomaly at epoch: | 24.5840° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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