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 26071.21522970 +.00000000 +00000-0 +79361-4 0 00000
2 24773 82.9253 168.5827 0025488 69.8489 354.0120 13.73972516 01
| Epoch (UTC): | 12 March 2026 05:09:55 |
| Eccentricity: | 0.0025488 |
| inclination: | 82.9253° |
| perigee height: | 967 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 168.5827° |
| argument of perigee: | 69.8489° |
| revolutions per day: | 13.73972516 |
| mean anomaly at epoch: | 354.0120° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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