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 06323U 26088.13733529 +.00000000 +00000-0 +81863-4 0 00004
2 06323 74.0790 246.5704 0018573 234.8610 125.0804 14.37482162 07
| Epoch (UTC): | 29 March 2026 03:17:45 |
| Eccentricity: | 0.0018573 |
| inclination: | 74.0790° |
| perigee height: | 754 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 246.5704° |
| argument of perigee: | 234.8610° |
| revolutions per day: | 14.37482162 |
| mean anomaly at epoch: | 125.0804° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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