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 58407U 26145.23337361 +.00000000 +00000-0 -28220-4 0 00002
2 58407 43.0031 340.1612 0000803 283.9988 76.0774 15.27580259 07
| Epoch (UTC): | 25 May 2026 05:36:03 |
| Eccentricity: | 0.0000803 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 340.1612° |
| argument of perigee: | 283.9988° |
| revolutions per day: | 15.27580259 |
| mean anomaly at epoch: | 76.0774° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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