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 26066.18845455 +.00000000 +00000-0 +65236-4 0 00006
2 14552 82.5261 332.0099 0018103 87.7848 272.5441 14.85858018 07
| Epoch (UTC): | 07 March 2026 04:31:22 |
| Eccentricity: | 0.0018103 |
| inclination: | 82.5261° |
| perigee height: | 598 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 332.0099° |
| argument of perigee: | 87.7848° |
| revolutions per day: | 14.85858018 |
| mean anomaly at epoch: | 272.5441° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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