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 57939U 26144.94772477 +.00000000 +00000-0 -37639-4 0 00003
2 57939 53.1610 30.2713 0001615 81.3627 278.7557 15.30180787 08
| Epoch (UTC): | 24 May 2026 22:44:43 |
| Eccentricity: | 0.0001615 |
| inclination: | 53.1610° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 30.2713° |
| argument of perigee: | 81.3627° |
| revolutions per day: | 15.30180787 |
| mean anomaly at epoch: | 278.7557° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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