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 26071.68555910 +.00000000 +00000-0 +46555-3 0 00008
2 32953 82.5007 55.4585 0019637 158.7134 201.4767 12.43176183 06
| Epoch (UTC): | 12 March 2026 16:27:12 |
| Eccentricity: | 0.0019637 |
| inclination: | 82.5007° |
| perigee height: | 1478 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 55.4585° |
| argument of perigee: | 158.7134° |
| revolutions per day: | 12.43176183 |
| mean anomaly at epoch: | 201.4767° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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