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 15755U 26158.74907387 +.00000000 +00000-0 +37541-4 0 00007
2 15755 71.1122 296.0322 0035253 355.4455 4.6345 14.21007461 00
| Epoch (UTC): | 07 June 2026 17:58:39 |
| Eccentricity: | 0.0035253 |
| inclination: | 71.1122° |
| perigee height: | 797 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 296.0322° |
| argument of perigee: | 355.4455° |
| revolutions per day: | 14.21007461 |
| mean anomaly at epoch: | 4.6345° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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