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 39019U 26145.64677338 +.00000000 +00000-0 +81220-4 0 00004
2 39019 98.1944 221.0085 0001396 101.9986 258.1370 14.58543861 01
| Epoch (UTC): | 25 May 2026 15:31:21 |
| Eccentricity: | 0.0001396 |
| inclination: | 98.1944° |
| perigee height: | 697 km |
| apogee height: | 699 km |
| right ascension of ascending node: | 221.0085° |
| argument of perigee: | 101.9986° |
| revolutions per day: | 14.58543861 |
| mean anomaly at epoch: | 258.1370° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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