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 58250U 26145.59379067 +.00000000 +00000-0 +41746-3 0 00002
2 58250 42.9999 211.0960 0001647 272.1607 87.9056 15.27810691 01
| Epoch (UTC): | 25 May 2026 14:15:03 |
| Eccentricity: | 0.0001647 |
| inclination: | 42.9999° |
| perigee height: | 481 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 211.0960° |
| argument of perigee: | 272.1607° |
| revolutions per day: | 15.27810691 |
| mean anomaly at epoch: | 87.9056° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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