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 58304U 26145.50442331 +.00000000 +00000-0 +43272-3 0 00004
2 58304 97.3927 236.4835 0005720 200.7563 159.3459 15.54062450 05
| Epoch (UTC): | 25 May 2026 12:06:22 |
| Eccentricity: | 0.0005720 |
| inclination: | 97.3927° |
| perigee height: | 401 km |
| apogee height: | 409 km |
| right ascension of ascending node: | 236.4835° |
| argument of perigee: | 200.7563° |
| revolutions per day: | 15.54062450 |
| mean anomaly at epoch: | 159.3459° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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