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 13154U 26088.13711243 +.00000000 +00000-0 +22114-3 0 00006
2 13154 81.1567 193.5381 0028589 260.1229 99.6768 15.10189093 00
| Epoch (UTC): | 29 March 2026 03:17:26 |
| Eccentricity: | 0.0028589 |
| inclination: | 81.1567° |
| perigee height: | 516 km |
| apogee height: | 555 km |
| right ascension of ascending node: | 193.5381° |
| argument of perigee: | 260.1229° |
| revolutions per day: | 15.10189093 |
| mean anomaly at epoch: | 99.6768° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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