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 58869U 26145.51579337 +.00000000 +00000-0 +75077-6 0 00009
2 58869 43.0015 171.4248 0001009 284.9158 75.1582 15.27568282 09
| Epoch (UTC): | 25 May 2026 12:22:44 |
| Eccentricity: | 0.0001009 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 171.4248° |
| argument of perigee: | 284.9158° |
| revolutions per day: | 15.27568282 |
| mean anomaly at epoch: | 75.1582° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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