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 57465U 26145.37497449 +.00000000 +00000-0 +17206-3 0 00004
2 57465 43.0025 263.1579 0001835 268.8179 91.2462 15.27575413 08
| Epoch (UTC): | 25 May 2026 08:59:57 |
| Eccentricity: | 0.0001835 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 263.1579° |
| argument of perigee: | 268.8179° |
| revolutions per day: | 15.27575413 |
| mean anomaly at epoch: | 91.2462° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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