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 58081U 26145.31352637 +.00000000 +00000-0 +81248-3 0 00009
2 58081 43.0043 7.7949 0001269 257.3156 102.7553 15.25111097 06
| Epoch (UTC): | 25 May 2026 07:31:28 |
| Eccentricity: | 0.0001269 |
| inclination: | 43.0043° |
| perigee height: | 490 km |
| apogee height: | 491 km |
| right ascension of ascending node: | 7.7949° |
| argument of perigee: | 257.3156° |
| revolutions per day: | 15.25111097 |
| mean anomaly at epoch: | 102.7553° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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