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 26069.99968979 +.00000000 +00000-0 +80993-4 0 00008
2 24773 82.9253 169.4836 0025522 73.0765 101.7423 13.73972294 00
| Epoch (UTC): | 10 March 2026 23:59:33 |
| Eccentricity: | 0.0025522 |
| inclination: | 82.9253° |
| perigee height: | 967 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 169.4836° |
| argument of perigee: | 73.0765° |
| revolutions per day: | 13.73972294 |
| mean anomaly at epoch: | 101.7423° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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