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 28058U 26145.31155911 +.00000000 +00000-0 +58514-4 0 00007
2 28058 98.5104 44.2121 0011293 250.9923 109.0046 14.48571604 02
| Epoch (UTC): | 25 May 2026 07:28:38 |
| Eccentricity: | 0.0011293 |
| inclination: | 98.5104° |
| perigee height: | 722 km |
| apogee height: | 738 km |
| right ascension of ascending node: | 44.2121° |
| argument of perigee: | 250.9923° |
| revolutions per day: | 14.48571604 |
| mean anomaly at epoch: | 109.0046° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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