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 19852U 26088.18707956 +.00000000 +00000-0 +34794-4 0 00006
2 19852 82.5177 257.0721 0018556 71.7476 288.5701 13.84168445 03
| Epoch (UTC): | 29 March 2026 04:29:23 |
| Eccentricity: | 0.0018556 |
| inclination: | 82.5177° |
| perigee height: | 936 km |
| apogee height: | 963 km |
| right ascension of ascending node: | 257.0721° |
| argument of perigee: | 71.7476° |
| revolutions per day: | 13.84168445 |
| mean anomaly at epoch: | 288.5701° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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