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 57346U 26145.52565586 +.00000000 +00000-0 +37885-4 0 00003
2 57346 43.0003 175.3940 0001225 282.2948 77.7766 15.27578024 02
| Epoch (UTC): | 25 May 2026 12:36:56 |
| Eccentricity: | 0.0001225 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 175.3940° |
| argument of perigee: | 282.2948° |
| revolutions per day: | 15.27578024 |
| mean anomaly at epoch: | 77.7766° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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