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 24971U 26066.22603816 +.00000000 +00000-0 +10895-3 0 00000
2 24971 98.8395 58.1020 0052337 166.9615 193.2937 14.35468740 03
| Epoch (UTC): | 07 March 2026 05:25:29 |
| Eccentricity: | 0.0052337 |
| inclination: | 98.8395° |
| perigee height: | 736 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 58.1020° |
| argument of perigee: | 166.9615° |
| revolutions per day: | 14.35468740 |
| mean anomaly at epoch: | 193.2937° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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