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 26087.98641950 +.00000000 +00000-0 +13832-3 0 00001
2 28373 98.6968 95.4087 0064327 234.0381 125.4835 14.48997296 04
| Epoch (UTC): | 28 March 2026 23:40:26 |
| Eccentricity: | 0.0064327 |
| inclination: | 98.6968° |
| perigee height: | 683 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 95.4087° |
| argument of perigee: | 234.0381° |
| revolutions per day: | 14.48997296 |
| mean anomaly at epoch: | 125.4835° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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