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 22578U 26088.09684231 +.00000000 +00000-0 +14663-3 0 00007
2 22578 71.0640 323.9849 0107337 354.0564 124.3843 14.53129236 01
| Epoch (UTC): | 29 March 2026 02:19:27 |
| Eccentricity: | 0.0107337 |
| inclination: | 71.0640° |
| perigee height: | 639 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 323.9849° |
| argument of perigee: | 354.0564° |
| revolutions per day: | 14.53129236 |
| mean anomaly at epoch: | 124.3843° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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