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 58067U 26145.50071382 +.00000000 +00000-0 +64942-4 0 00002
2 58067 43.0008 313.5533 0001288 277.3231 82.7474 15.27581832 04
| Epoch (UTC): | 25 May 2026 12:01:01 |
| Eccentricity: | 0.0001288 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 313.5533° |
| argument of perigee: | 277.3231° |
| revolutions per day: | 15.27581832 |
| mean anomaly at epoch: | 82.7474° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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