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 26073.93895712 +.00000000 +00000-0 +56666-3 0 00009
2 32953 82.5006 54.0562 0019715 153.8663 206.3416 12.43176404 06
| Epoch (UTC): | 14 March 2026 22:32:05 |
| Eccentricity: | 0.0019715 |
| inclination: | 82.5006° |
| perigee height: | 1478 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 54.0562° |
| argument of perigee: | 153.8663° |
| revolutions per day: | 12.43176404 |
| mean anomaly at epoch: | 206.3416° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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