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 28373U 26142.46868623 +.00000000 +00000-0 +95233-4 0 00000
2 28373 98.6941 151.5457 0066388 70.4064 290.4279 14.49045336 04
| Epoch (UTC): | 22 May 2026 11:14:54 |
| Eccentricity: | 0.0066388 |
| inclination: | 98.6941° |
| perigee height: | 682 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 151.5457° |
| argument of perigee: | 70.4064° |
| revolutions per day: | 14.49045336 |
| mean anomaly at epoch: | 290.4279° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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