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 26076.08780525 +.00000000 +00000-0 +45528-4 0 00004
2 14552 82.5248 322.7075 0017857 57.7818 302.5127 14.85868853 04
| Epoch (UTC): | 17 March 2026 02:06:26 |
| Eccentricity: | 0.0017857 |
| inclination: | 82.5248° |
| perigee height: | 598 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 322.7075° |
| argument of perigee: | 57.7818° |
| revolutions per day: | 14.85868853 |
| mean anomaly at epoch: | 302.5127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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