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 26038.12600909 +.00000000 +00000-0 +64723-5 0 00008
2 32953 82.4987 76.3468 0018539 232.9871 126.9512 12.43174879 06
| Epoch (UTC): | 07 February 2026 03:01:27 |
| Eccentricity: | 0.0018539 |
| inclination: | 82.4987° |
| perigee height: | 1479 km |
| apogee height: | 1508 km |
| right ascension of ascending node: | 76.3468° |
| argument of perigee: | 232.9871° |
| revolutions per day: | 12.43174879 |
| mean anomaly at epoch: | 126.9512° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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