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 57387U 26145.60343873 +.00000000 +00000-0 +97922-4 0 00008
2 57387 99.5097 158.0947 0005235 183.5146 176.6039 15.06577674 08
| Epoch (UTC): | 25 May 2026 14:28:57 |
| Eccentricity: | 0.0005235 |
| inclination: | 99.5097° |
| perigee height: | 543 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 158.0947° |
| argument of perigee: | 183.5146° |
| revolutions per day: | 15.06577674 |
| mean anomaly at epoch: | 176.6039° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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