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 57886U 26144.66712074 +.00000000 +00000-0 +37289-3 0 00009
2 57886 35.0034 348.3724 0001744 94.8423 265.2491 15.23194640 02
| Epoch (UTC): | 24 May 2026 16:00:39 |
| Eccentricity: | 0.0001744 |
| inclination: | 35.0034° |
| perigee height: | 495 km |
| apogee height: | 497 km |
| right ascension of ascending node: | 348.3724° |
| argument of perigee: | 94.8423° |
| revolutions per day: | 15.23194640 |
| mean anomaly at epoch: | 265.2491° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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