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 57414U 26145.66668980 +.00000000 +00000-0 +23273-2 0 00000
2 57414 43.0008 174.5868 0001375 288.4412 73.5742 15.35755582 06
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001375 |
| inclination: | 43.0008° |
| perigee height: | 458 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 174.5868° |
| argument of perigee: | 288.4412° |
| revolutions per day: | 15.35755582 |
| mean anomaly at epoch: | 73.5742° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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