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 26150.87616073 +.00000000 +00000-0 +35664-5 0 00006
2 32953 82.5056 6.2107 0019600 352.3790 7.6989 12.43178433 06
| Epoch (UTC): | 30 May 2026 21:01:40 |
| Eccentricity: | 0.0019600 |
| inclination: | 82.5056° |
| perigee height: | 1478 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 6.2107° |
| argument of perigee: | 352.3790° |
| revolutions per day: | 12.43178433 |
| mean anomaly at epoch: | 7.6989° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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