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 19210U 26076.21918492 +.00000000 +00000-0 +21416-3 0 00000
2 19210 82.5102 150.6748 0012667 98.9424 261.3250 15.28653980 08
| Epoch (UTC): | 17 March 2026 05:15:37 |
| Eccentricity: | 0.0012667 |
| inclination: | 82.5102° |
| perigee height: | 471 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 150.6748° |
| argument of perigee: | 98.9424° |
| revolutions per day: | 15.28653980 |
| mean anomaly at epoch: | 261.3250° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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