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 26022.46523904 +.00000000 +00000-0 +15830-3 0 00003
2 06324 74.0757 40.1722 0007127 90.5420 269.6554 14.45240473 01
| Epoch (UTC): | 22 January 2026 11:09:56 |
| Eccentricity: | 0.0007127 |
| inclination: | 74.0757° |
| perigee height: | 736 km |
| apogee height: | 746 km |
| right ascension of ascending node: | 40.1722° |
| argument of perigee: | 90.5420° |
| revolutions per day: | 14.45240473 |
| mean anomaly at epoch: | 269.6554° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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