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 32954U 26145.65926279 +.00000000 +00000-0 +71548-3 0 00008
2 32954 82.5042 11.4735 0021162 20.9297 359.2282 12.42759240 05
| Epoch (UTC): | 25 May 2026 15:49:20 |
| Eccentricity: | 0.0021162 |
| inclination: | 82.5042° |
| perigee height: | 1478 km |
| apogee height: | 1512 km |
| right ascension of ascending node: | 11.4735° |
| argument of perigee: | 20.9297° |
| revolutions per day: | 12.42759240 |
| mean anomaly at epoch: | 359.2282° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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