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 58681U 26145.32677316 +.00000000 +00000-0 +40301-4 0 00006
2 58681 43.0008 12.6143 0001128 279.5706 80.5018 15.27579850 01
| Epoch (UTC): | 25 May 2026 07:50:33 |
| Eccentricity: | 0.0001128 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 12.6143° |
| argument of perigee: | 279.5706° |
| revolutions per day: | 15.27579850 |
| mean anomaly at epoch: | 80.5018° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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