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 26046.17386372 +.00000000 +00000-0 +19495-3 0 00001
2 32953 82.4990 71.3383 0018765 214.8571 145.1281 12.43175021 04
| Epoch (UTC): | 15 February 2026 04:10:21 |
| Eccentricity: | 0.0018765 |
| inclination: | 82.4990° |
| perigee height: | 1478 km |
| apogee height: | 1508 km |
| right ascension of ascending node: | 71.3383° |
| argument of perigee: | 214.8571° |
| revolutions per day: | 12.43175021 |
| mean anomaly at epoch: | 145.1281° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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