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 26100.49683458 +.00000000 +00000-0 +52677-3 0 00001
2 32953 82.5060 37.5369 0020516 97.6504 262.6907 12.43177536 04
| Epoch (UTC): | 10 April 2026 11:55:26 |
| Eccentricity: | 0.0020516 |
| inclination: | 82.5060° |
| perigee height: | 1477 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 37.5369° |
| argument of perigee: | 97.6504° |
| revolutions per day: | 12.43177536 |
| mean anomaly at epoch: | 262.6907° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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