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 20528U 26103.24646008 +.00000000 +00000-0 +35683-4 0 00001
2 20528 82.9394 202.5882 0033066 71.4713 317.6705 13.73149220 03
| Epoch (UTC): | 13 April 2026 05:54:54 |
| Eccentricity: | 0.0033066 |
| inclination: | 82.9394° |
| perigee height: | 964 km |
| apogee height: | 1013 km |
| right ascension of ascending node: | 202.5882° |
| argument of perigee: | 71.4713° |
| revolutions per day: | 13.73149220 |
| mean anomaly at epoch: | 317.6705° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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