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 58639U 26145.30087140 +.00000000 +00000-0 +30186-4 0 00007
2 58639 43.0046 354.8158 0001165 259.7943 100.2778 15.27581628 06
| Epoch (UTC): | 25 May 2026 07:13:15 |
| Eccentricity: | 0.0001165 |
| inclination: | 43.0046° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 354.8158° |
| argument of perigee: | 259.7943° |
| revolutions per day: | 15.27581628 |
| mean anomaly at epoch: | 100.2778° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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