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 26070.83378765 +.00000000 +00000-0 +11101-3 0 00007
2 28096 63.6789 280.9127 0073294 117.4014 243.4493 13.41063357 00
| Epoch (UTC): | 11 March 2026 20:00:39 |
| Eccentricity: | 0.0073294 |
| inclination: | 63.6789° |
| perigee height: | 1050 km |
| apogee height: | 1160 km |
| right ascension of ascending node: | 280.9127° |
| argument of perigee: | 117.4014° |
| revolutions per day: | 13.41063357 |
| mean anomaly at epoch: | 243.4493° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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