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 24827U 26137.84339257 +.00000000 +00000-0 -97748-3 0 00005
2 24827 63.3054 256.7456 1090451 69.3419 94.8638 11.07977140 08
| Epoch (UTC): | 17 May 2026 20:14:29 |
| Eccentricity: | 0.1090451 |
| inclination: | 63.3054° |
| perigee height: | 1194 km |
| apogee height: | 3048 km |
| right ascension of ascending node: | 256.7456° |
| argument of perigee: | 69.3419° |
| revolutions per day: | 11.07977140 |
| mean anomaly at epoch: | 94.8638° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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