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 28096U 26067.03079314 +.00000000 +00000-0 +11074-3 0 00002
2 28096 63.6793 290.5141 0073434 117.7927 243.0569 13.41062883 03
| Epoch (UTC): | 08 March 2026 00:44:20 |
| Eccentricity: | 0.0073434 |
| inclination: | 63.6793° |
| perigee height: | 1050 km |
| apogee height: | 1160 km |
| right ascension of ascending node: | 290.5141° |
| argument of perigee: | 117.7927° |
| revolutions per day: | 13.41062883 |
| mean anomaly at epoch: | 243.0569° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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