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 26088.18364507 +.00000000 +00000-0 +50774-3 0 00009
2 32953 82.5033 45.1937 0020215 123.4599 236.8417 12.43176873 00
| Epoch (UTC): | 29 March 2026 04:24:26 |
| Eccentricity: | 0.0020215 |
| inclination: | 82.5033° |
| perigee height: | 1477 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 45.1937° |
| argument of perigee: | 123.4599° |
| revolutions per day: | 12.43176873 |
| mean anomaly at epoch: | 236.8417° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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