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 22783U 26088.16506579 +.00000000 +00000-0 +32514-4 0 00007
2 22783 82.5556 1.4557 0024104 74.1434 286.2380 13.83890563 06
| Epoch (UTC): | 29 March 2026 03:57:41 |
| Eccentricity: | 0.0024104 |
| inclination: | 82.5556° |
| perigee height: | 932 km |
| apogee height: | 968 km |
| right ascension of ascending node: | 1.4557° |
| argument of perigee: | 74.1434° |
| revolutions per day: | 13.83890563 |
| mean anomaly at epoch: | 286.2380° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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