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 60053U 26145.24762205 +.00000000 +00000-0 +16871-4 0 00000
2 60053 53.1604 82.6985 0001275 86.3082 273.8064 15.30197700 08
| Epoch (UTC): | 25 May 2026 05:56:34 |
| Eccentricity: | 0.0001275 |
| inclination: | 53.1604° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 82.6985° |
| argument of perigee: | 86.3082° |
| revolutions per day: | 15.30197700 |
| mean anomaly at epoch: | 273.8064° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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