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 26066.99656802 +.00000000 +00000-0 +77632-4 0 00004
2 14552 82.5260 331.2506 0018105 85.3280 275.0004 14.85859659 01
| Epoch (UTC): | 07 March 2026 23:55:03 |
| Eccentricity: | 0.0018105 |
| inclination: | 82.5260° |
| perigee height: | 598 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 331.2506° |
| argument of perigee: | 85.3280° |
| revolutions per day: | 14.85859659 |
| mean anomaly at epoch: | 275.0004° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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