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 57672U 26145.35019450 +.00000000 +00000-0 +25040-4 0 00000
2 57672 53.1596 210.8673 0000842 93.7250 266.3847 15.30192893 02
| Epoch (UTC): | 25 May 2026 08:24:16 |
| Eccentricity: | 0.0000842 |
| inclination: | 53.1596° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 210.8673° |
| argument of perigee: | 93.7250° |
| revolutions per day: | 15.30192893 |
| mean anomaly at epoch: | 266.3847° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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