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 60190U 26145.30346462 +.00000000 +00000-0 +73255-5 0 00002
2 60190 53.1588 143.8352 0001150 72.5720 287.5423 15.69703406 06
| Epoch (UTC): | 25 May 2026 07:16:59 |
| Eccentricity: | 0.0001150 |
| inclination: | 53.1588° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 143.8352° |
| argument of perigee: | 72.5720° |
| revolutions per day: | 15.69703406 |
| mean anomaly at epoch: | 287.5423° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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