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 10820U 26072.80339853 +.00000000 +00000-0 +19645-3 0 00008
2 10820 98.4535 269.1939 0008182 273.3692 86.6560 14.37993655 00
| Epoch (UTC): | 13 March 2026 19:16:53 |
| Eccentricity: | 0.0008182 |
| inclination: | 98.4535° |
| perigee height: | 759 km |
| apogee height: | 771 km |
| right ascension of ascending node: | 269.1939° |
| argument of perigee: | 273.3692° |
| revolutions per day: | 14.37993655 |
| mean anomaly at epoch: | 86.6560° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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