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 26101.54305222 +.00000000 +00000-0 +77037-3 0 00005
2 32953 82.5059 36.8863 0020544 95.5266 264.8157 12.43177830 04
| Epoch (UTC): | 11 April 2026 13:01:59 |
| Eccentricity: | 0.0020544 |
| inclination: | 82.5059° |
| perigee height: | 1477 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 36.8863° |
| argument of perigee: | 95.5266° |
| revolutions per day: | 12.43177830 |
| mean anomaly at epoch: | 264.8157° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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