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 58019U 26145.58437213 +.00000000 +00000-0 +10381-2 0 00002
2 58019 97.5550 234.4073 0002445 140.1253 220.0175 15.44474174 08
| Epoch (UTC): | 25 May 2026 14:01:29 |
| Eccentricity: | 0.0002445 |
| inclination: | 97.5550° |
| perigee height: | 431 km |
| apogee height: | 435 km |
| right ascension of ascending node: | 234.4073° |
| argument of perigee: | 140.1253° |
| revolutions per day: | 15.44474174 |
| mean anomaly at epoch: | 220.0175° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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