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 59157U 26145.38380463 +.00000000 +00000-0 +17674-3 0 00001
2 59157 42.9997 37.4546 0001422 266.7733 93.2956 15.27588196 07
| Epoch (UTC): | 25 May 2026 09:12:40 |
| Eccentricity: | 0.0001422 |
| inclination: | 42.9997° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 37.4546° |
| argument of perigee: | 266.7733° |
| revolutions per day: | 15.27588196 |
| mean anomaly at epoch: | 93.2956° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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