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 24594U 26088.15891194 +.00000000 +00000-0 +85013-3 0 00009
2 24594 81.4464 73.7349 0448421 192.4222 166.5606 14.11712786 09
| Epoch (UTC): | 29 March 2026 03:48:49 |
| Eccentricity: | 0.0448421 |
| inclination: | 81.4464° |
| perigee height: | 529 km |
| apogee height: | 1178 km |
| right ascension of ascending node: | 73.7349° |
| argument of perigee: | 192.4222° |
| revolutions per day: | 14.11712786 |
| mean anomaly at epoch: | 166.5606° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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