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 24773U 26068.37555850 +.00000000 +00000-0 +85273-4 0 00005
2 24773 82.9253 170.6874 0025539 77.3451 348.5541 13.73972003 03
| Epoch (UTC): | 09 March 2026 09:00:48 |
| Eccentricity: | 0.0025539 |
| inclination: | 82.9253° |
| perigee height: | 967 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 170.6874° |
| argument of perigee: | 77.3451° |
| revolutions per day: | 13.73972003 |
| mean anomaly at epoch: | 348.5541° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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