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 60307U 26145.32911270 +.00000000 +00000-0 +12225-4 0 00008
2 60307 53.1587 128.2365 0001112 72.2646 287.8493 15.69705335 01
| Epoch (UTC): | 25 May 2026 07:53:55 |
| Eccentricity: | 0.0001112 |
| inclination: | 53.1587° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 128.2365° |
| argument of perigee: | 72.2646° |
| revolutions per day: | 15.69705335 |
| mean anomaly at epoch: | 287.8493° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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