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 20827U 26129.33947963 +.00000000 +00000-0 +19081-4 0 00009
2 20827 82.5299 233.3724 0104745 83.0094 278.2966 13.84648822 01
| Epoch (UTC): | 09 May 2026 08:08:51 |
| Eccentricity: | 0.0104745 |
| inclination: | 82.5299° |
| perigee height: | 871 km |
| apogee height: | 1024 km |
| right ascension of ascending node: | 233.3724° |
| argument of perigee: | 83.0094° |
| revolutions per day: | 13.84648822 |
| mean anomaly at epoch: | 278.2966° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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