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 58308U 26145.22957947 +.00000000 +00000-0 +48614-3 0 00006
2 58308 97.3854 236.4701 0005966 195.9073 164.1995 15.56054969 00
| Epoch (UTC): | 25 May 2026 05:30:35 |
| Eccentricity: | 0.0005966 |
| inclination: | 97.3854° |
| perigee height: | 395 km |
| apogee height: | 403 km |
| right ascension of ascending node: | 236.4701° |
| argument of perigee: | 195.9073° |
| revolutions per day: | 15.56054969 |
| mean anomaly at epoch: | 164.1995° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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