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 58394U 26145.34231301 +.00000000 +00000-0 -20742-5 0 00008
2 58394 53.1609 4.4076 0001031 90.5381 269.5740 15.34380123 00
| Epoch (UTC): | 25 May 2026 08:12:55 |
| Eccentricity: | 0.0001031 |
| inclination: | 53.1609° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 4.4076° |
| argument of perigee: | 90.5381° |
| revolutions per day: | 15.34380123 |
| mean anomaly at epoch: | 269.5740° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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