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 60112U 26145.13678101 +.00000000 +00000-0 +54563-4 0 00005
2 60112 53.1607 41.8339 0001130 85.2357 274.8772 15.30196349 05
| Epoch (UTC): | 25 May 2026 03:16:57 |
| Eccentricity: | 0.0001130 |
| inclination: | 53.1607° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 41.8339° |
| argument of perigee: | 85.2357° |
| revolutions per day: | 15.30196349 |
| mean anomaly at epoch: | 274.8772° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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