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 59957U 26145.24216192 +.00000000 +00000-0 +14386-4 0 00009
2 59957 53.1600 233.5715 0001187 91.8910 268.2244 15.69711169 07
| Epoch (UTC): | 25 May 2026 05:48:42 |
| Eccentricity: | 0.0001187 |
| inclination: | 53.1600° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 233.5715° |
| argument of perigee: | 91.8910° |
| revolutions per day: | 15.69711169 |
| mean anomaly at epoch: | 268.2244° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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