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 26819U 26088.00739617 +.00000000 +00000-0 +18651-3 0 00000
2 26819 82.9204 259.8559 0022464 200.9372 280.0797 13.75939347 01
| Epoch (UTC): | 29 March 2026 00:10:39 |
| Eccentricity: | 0.0022464 |
| inclination: | 82.9204° |
| perigee height: | 962 km |
| apogee height: | 995 km |
| right ascension of ascending node: | 259.8559° |
| argument of perigee: | 200.9372° |
| revolutions per day: | 13.75939347 |
| mean anomaly at epoch: | 280.0797° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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