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 61919U 26145.17144088 +.00000000 +00000-0 +58476-3 0 00003
2 61919 43.0005 209.4157 0002939 277.4670 82.5847 15.27596360 02
| Epoch (UTC): | 25 May 2026 04:06:52 |
| Eccentricity: | 0.0002939 |
| inclination: | 43.0005° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 209.4157° |
| argument of perigee: | 277.4670° |
| revolutions per day: | 15.27596360 |
| mean anomaly at epoch: | 82.5847° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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