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 58502U 26145.60001404 +.00000000 +00000-0 +13485-3 0 00000
2 58502 97.4383 163.6994 0010480 350.0950 10.0084 15.33099937 01
| Epoch (UTC): | 25 May 2026 14:24:01 |
| Eccentricity: | 0.0010480 |
| inclination: | 97.4383° |
| perigee height: | 459 km |
| apogee height: | 474 km |
| right ascension of ascending node: | 163.6994° |
| argument of perigee: | 350.0950° |
| revolutions per day: | 15.33099937 |
| mean anomaly at epoch: | 10.0084° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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