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 14552U 26073.66348142 +.00000000 +00000-0 +57941-4 0 00002
2 14552 82.5251 324.9859 0017973 65.1515 295.1568 14.85867187 03
| Epoch (UTC): | 14 March 2026 15:55:24 |
| Eccentricity: | 0.0017973 |
| inclination: | 82.5251° |
| perigee height: | 598 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 324.9859° |
| argument of perigee: | 65.1515° |
| revolutions per day: | 14.85867187 |
| mean anomaly at epoch: | 295.1568° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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