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 58253U 26145.53533182 +.00000000 +00000-0 +00000-0 0 00004
2 58253 0.0519 100.8406 0002762 330.4967 120.0072 1.00270178 06
| Epoch (UTC): | 25 May 2026 12:50:52 |
| Eccentricity: | 0.0002762 |
| inclination: | 0.0519° |
| perigee height: | 35775 km |
| apogee height: | 35799 km |
| right ascension of ascending node: | 100.8406° |
| argument of perigee: | 330.4967° |
| revolutions per day: | 1.00270178 |
| mean anomaly at epoch: | 120.0072° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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