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 59423U 26145.09835528 +.00000000 +00000-0 +25676-4 0 00004
2 59423 53.1592 77.2398 0001230 124.1400 235.9735 15.69707458 00
| Epoch (UTC): | 25 May 2026 02:21:37 |
| Eccentricity: | 0.0001230 |
| inclination: | 53.1592° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 77.2398° |
| argument of perigee: | 124.1400° |
| revolutions per day: | 15.69707458 |
| mean anomaly at epoch: | 235.9735° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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