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 58055U 26145.51855911 +.00000000 +00000-0 +17885-4 0 00002
2 58055 43.0036 312.8458 0001870 258.4127 101.6515 15.27576733 02
| Epoch (UTC): | 25 May 2026 12:26:43 |
| Eccentricity: | 0.0001870 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 312.8458° |
| argument of perigee: | 258.4127° |
| revolutions per day: | 15.27576733 |
| mean anomaly at epoch: | 101.6515° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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