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 24292U 26105.76949324 +.00000000 +00000-0 +14558-2 0 00005
2 24292 62.6661 187.9755 5585114 268.6826 30.3318 4.14738571 05
| Epoch (UTC): | 15 April 2026 18:28:04 |
| Eccentricity: | 0.5585114 |
| inclination: | 62.6661° |
| perigee height: | 846 km |
| apogee height: | 19125 km |
| right ascension of ascending node: | 187.9755° |
| argument of perigee: | 268.6826° |
| revolutions per day: | 4.14738571 |
| mean anomaly at epoch: | 30.3318° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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