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 28352U 26074.04519037 +.00000000 +00000-0 -75729-4 0 00006
2 28352 70.9991 296.2744 0012102 277.1388 82.8357 14.12143314 00
| Epoch (UTC): | 15 March 2026 01:05:04 |
| Eccentricity: | 0.0012102 |
| inclination: | 70.9991° |
| perigee height: | 843 km |
| apogee height: | 861 km |
| right ascension of ascending node: | 296.2744° |
| argument of perigee: | 277.1388° |
| revolutions per day: | 14.12143314 |
| mean anomaly at epoch: | 82.8357° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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