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 52336U 26145.51910388 +.00000000 +00000-0 +51730-4 0 00005
2 52336 53.2122 224.0152 0001146 73.3890 286.7227 15.08837313 07
| Epoch (UTC): | 25 May 2026 12:27:30 |
| Eccentricity: | 0.0001146 |
| inclination: | 53.2122° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 224.0152° |
| argument of perigee: | 73.3890° |
| revolutions per day: | 15.08837313 |
| mean anomaly at epoch: | 286.7227° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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