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 19659U 26088.23166873 +.00000000 +00000-0 +81502-4 0 00003
2 19659 71.0363 174.8812 0186415 4.7532 25.0368 13.77391210 07
| Epoch (UTC): | 29 March 2026 05:33:36 |
| Eccentricity: | 0.0186415 |
| inclination: | 71.0363° |
| perigee height: | 836 km |
| apogee height: | 1110 km |
| right ascension of ascending node: | 174.8812° |
| argument of perigee: | 4.7532° |
| revolutions per day: | 13.77391210 |
| mean anomaly at epoch: | 25.0368° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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