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 57874U 26145.45749815 +.00000000 +00000-0 +19624-4 0 00001
2 57874 43.0006 185.9100 0001343 268.2498 91.8200 15.27575813 04
| Epoch (UTC): | 25 May 2026 10:58:47 |
| Eccentricity: | 0.0001343 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 185.9100° |
| argument of perigee: | 268.2498° |
| revolutions per day: | 15.27575813 |
| mean anomaly at epoch: | 91.8200° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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