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 58990U 26145.52874513 +.00000000 +00000-0 +00000-0 0 00007
2 58990 0.0315 250.0372 0001494 162.0042 103.4832 1.00272447 02
| Epoch (UTC): | 25 May 2026 12:41:23 |
| Eccentricity: | 0.0001494 |
| inclination: | 0.0315° |
| perigee height: | 35780 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 250.0372° |
| argument of perigee: | 162.0042° |
| revolutions per day: | 1.00272447 |
| mean anomaly at epoch: | 103.4832° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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