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 32052U 26103.66634663 +.00000000 +00000-0 +41201-4 0 00009
2 32052 82.9781 253.4272 0039437 56.9006 303.5926 13.75161870 03
| Epoch (UTC): | 13 April 2026 15:59:32 |
| Eccentricity: | 0.0039437 |
| inclination: | 82.9781° |
| perigee height: | 952 km |
| apogee height: | 1010 km |
| right ascension of ascending node: | 253.4272° |
| argument of perigee: | 56.9006° |
| revolutions per day: | 13.75161870 |
| mean anomaly at epoch: | 303.5926° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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