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 57391U 26145.54617118 +.00000000 +00000-0 +62091-3 0 00000
2 57391 99.4491 177.7910 0008093 117.0465 243.1600 15.38485226 09
| Epoch (UTC): | 25 May 2026 13:06:29 |
| Eccentricity: | 0.0008093 |
| inclination: | 99.4491° |
| perigee height: | 445 km |
| apogee height: | 456 km |
| right ascension of ascending node: | 177.7910° |
| argument of perigee: | 117.0465° |
| revolutions per day: | 15.38485226 |
| mean anomaly at epoch: | 243.1600° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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