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 60191U 26145.23489595 +.00000000 +00000-0 -15996-4 0 00008
2 60191 53.1581 144.1136 0001311 81.1420 278.9746 15.69688756 08
| Epoch (UTC): | 25 May 2026 05:38:15 |
| Eccentricity: | 0.0001311 |
| inclination: | 53.1581° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 144.1136° |
| argument of perigee: | 81.1420° |
| revolutions per day: | 15.69688756 |
| mean anomaly at epoch: | 278.9746° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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