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 26064.71916830 +.00000000 +00000-0 +93936-4 0 00005
2 28096 63.6797 296.3499 0073477 118.0488 242.7995 13.41062478 09
| Epoch (UTC): | 05 March 2026 17:15:36 |
| Eccentricity: | 0.0073477 |
| inclination: | 63.6797° |
| perigee height: | 1050 km |
| apogee height: | 1160 km |
| right ascension of ascending node: | 296.3499° |
| argument of perigee: | 118.0488° |
| revolutions per day: | 13.41062478 |
| mean anomaly at epoch: | 242.7995° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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