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 20855U 26076.19780211 +.00000000 +00000-0 -51946-6 0 00005
2 20855 98.8231 59.4730 0024636 37.7006 332.9968 14.09162494 05
| Epoch (UTC): | 17 March 2026 04:44:50 |
| Eccentricity: | 0.0024636 |
| inclination: | 98.8231° |
| perigee height: | 844 km |
| apogee height: | 880 km |
| right ascension of ascending node: | 59.4730° |
| argument of perigee: | 37.7006° |
| revolutions per day: | 14.09162494 |
| mean anomaly at epoch: | 332.9968° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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