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 58557U 26145.48535691 +.00000000 +00000-0 +30349-3 0 00004
2 58557 35.0008 200.1683 0005294 117.2403 242.8852 15.23105375 09
| Epoch (UTC): | 25 May 2026 11:38:54 |
| Eccentricity: | 0.0005294 |
| inclination: | 35.0008° |
| perigee height: | 493 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 200.1683° |
| argument of perigee: | 117.2403° |
| revolutions per day: | 15.23105375 |
| mean anomaly at epoch: | 242.8852° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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