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 58297U 26145.42578839 +.00000000 +00000-0 +63242-3 0 00008
2 58297 97.3810 202.0566 0004663 138.6924 221.4658 15.08634795 00
| Epoch (UTC): | 25 May 2026 10:13:08 |
| Eccentricity: | 0.0004663 |
| inclination: | 97.3810° |
| perigee height: | 537 km |
| apogee height: | 544 km |
| right ascension of ascending node: | 202.0566° |
| argument of perigee: | 138.6924° |
| revolutions per day: | 15.08634795 |
| mean anomaly at epoch: | 221.4658° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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