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 20480U 26154.60440579 +.00000000 +00000-0 +73620-4 0 00002
2 20480 99.0730 80.0377 0540109 175.3384 185.3043 12.83489551 09
| Epoch (UTC): | 03 June 2026 14:30:20 |
| Eccentricity: | 0.0540109 |
| inclination: | 99.0730° |
| perigee height: | 911 km |
| apogee height: | 1744 km |
| right ascension of ascending node: | 80.0377° |
| argument of perigee: | 175.3384° |
| revolutions per day: | 12.83489551 |
| mean anomaly at epoch: | 185.3043° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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