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 58052U 26145.50457741 +.00000000 +00000-0 +10808-4 0 00005
2 58052 43.0016 313.5983 0001432 274.7515 85.3173 15.27572203 00
| Epoch (UTC): | 25 May 2026 12:06:35 |
| Eccentricity: | 0.0001432 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 313.5983° |
| argument of perigee: | 274.7515° |
| revolutions per day: | 15.27572203 |
| mean anomaly at epoch: | 85.3173° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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