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 26145.64508639 +.00000000 +00000-0 +14005-3 0 00007
2 32953 82.5059 9.4635 0019837 3.6591 356.4630 12.43178412 02
| Epoch (UTC): | 25 May 2026 15:28:55 |
| Eccentricity: | 0.0019837 |
| inclination: | 82.5059° |
| perigee height: | 1478 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 9.4635° |
| argument of perigee: | 3.6591° |
| revolutions per day: | 12.43178412 |
| mean anomaly at epoch: | 356.4630° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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