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 58949U 26145.43374404 +.00000000 +00000-0 +29365-4 0 00004
2 58949 53.1622 313.4734 0001277 100.3505 259.7640 15.30191380 06
| Epoch (UTC): | 25 May 2026 10:24:35 |
| Eccentricity: | 0.0001277 |
| inclination: | 53.1622° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 313.4734° |
| argument of perigee: | 100.3505° |
| revolutions per day: | 15.30191380 |
| mean anomaly at epoch: | 259.7640° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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