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 24834U 26053.01012163 +.00000000 +00000-0 +00000-0 0 00004
2 24834 15.5955 6.9076 0104832 235.9878 292.0316 0.96051439 01
| Epoch (UTC): | 22 February 2026 00:14:34 |
| Eccentricity: | 0.0104832 |
| inclination: | 15.5955° |
| perigee height: | 36558 km |
| apogee height: | 37468 km |
| right ascension of ascending node: | 6.9076° |
| argument of perigee: | 235.9878° |
| revolutions per day: | 0.96051439 |
| mean anomaly at epoch: | 292.0316° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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