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 60052U 26145.24128687 +.00000000 +00000-0 +50401-4 0 00006
2 60052 53.1600 82.6590 0001320 93.2524 266.8627 15.30198532 05
| Epoch (UTC): | 25 May 2026 05:47:27 |
| Eccentricity: | 0.0001320 |
| inclination: | 53.1600° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 82.6590° |
| argument of perigee: | 93.2524° |
| revolutions per day: | 15.30198532 |
| mean anomaly at epoch: | 266.8627° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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