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 32953U 26073.21465097 +.00000000 +00000-0 -16450-4 0 00008
2 32953 82.5007 54.5070 0019680 155.4434 204.7587 12.43175939 04
| Epoch (UTC): | 14 March 2026 05:09:05 |
| Eccentricity: | 0.0019680 |
| inclination: | 82.5007° |
| perigee height: | 1478 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 54.5070° |
| argument of perigee: | 155.4434° |
| revolutions per day: | 12.43175939 |
| mean anomaly at epoch: | 204.7587° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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