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 26159.48731139 +.00000000 +00000-0 +48714-4 0 00002
2 32953 82.5048 0.8529 0019234 333.4810 26.5284 12.43178883 08
| Epoch (UTC): | 08 June 2026 11:41:43 |
| Eccentricity: | 0.0019234 |
| inclination: | 82.5048° |
| perigee height: | 1478 km |
| apogee height: | 1508 km |
| right ascension of ascending node: | 0.8529° |
| argument of perigee: | 333.4810° |
| revolutions per day: | 12.43178883 |
| mean anomaly at epoch: | 26.5284° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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