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 26100.25539978 +.00000000 +00000-0 -20581-4 0 00003
2 32953 82.5061 37.6871 0020520 98.1757 262.1652 12.43177251 01
| Epoch (UTC): | 10 April 2026 06:07:46 |
| Eccentricity: | 0.0020520 |
| inclination: | 82.5061° |
| perigee height: | 1477 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 37.6871° |
| argument of perigee: | 98.1757° |
| revolutions per day: | 12.43177251 |
| mean anomaly at epoch: | 262.1652° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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