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 26044.72110240 +.00000000 +00000-0 +23149-4 0 00008
2 20827 82.5297 300.8357 0102692 321.1152 38.2652 13.84644191 02
| Epoch (UTC): | 13 February 2026 17:18:23 |
| Eccentricity: | 0.0102692 |
| inclination: | 82.5297° |
| perigee height: | 872 km |
| apogee height: | 1023 km |
| right ascension of ascending node: | 300.8357° |
| argument of perigee: | 321.1152° |
| revolutions per day: | 13.84644191 |
| mean anomaly at epoch: | 38.2652° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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