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 58164U 26145.51009992 +.00000000 +00000-0 +89632-4 0 00002
2 58164 53.1613 222.5950 0000598 78.8788 281.2281 15.31695280 02
| Epoch (UTC): | 25 May 2026 12:14:32 |
| Eccentricity: | 0.0000598 |
| inclination: | 53.1613° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 222.5950° |
| argument of perigee: | 78.8788° |
| revolutions per day: | 15.31695280 |
| mean anomaly at epoch: | 281.2281° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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