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 60136U 26144.92022073 +.00000000 +00000-0 +19994-2 0 00005
2 60136 53.1614 326.1149 0001455 110.9020 249.2137 15.30655950 09
| Epoch (UTC): | 24 May 2026 22:05:07 |
| Eccentricity: | 0.0001455 |
| inclination: | 53.1614° |
| perigee height: | 473 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 326.1149° |
| argument of perigee: | 110.9020° |
| revolutions per day: | 15.30655950 |
| mean anomaly at epoch: | 249.2137° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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