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 57604U 26145.31052426 +.00000000 +00000-0 -19728-3 0 00007
2 57604 42.9999 8.9468 0001285 266.5696 93.5009 15.27592043 01
| Epoch (UTC): | 25 May 2026 07:27:09 |
| Eccentricity: | 0.0001285 |
| inclination: | 42.9999° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 8.9468° |
| argument of perigee: | 266.5696° |
| revolutions per day: | 15.27592043 |
| mean anomaly at epoch: | 93.5009° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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