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 57844U 26145.37039008 +.00000000 +00000-0 -48250-4 0 00003
2 57844 53.1615 287.5666 0001206 97.7004 262.4134 15.30177562 06
| Epoch (UTC): | 25 May 2026 08:53:21 |
| Eccentricity: | 0.0001206 |
| inclination: | 53.1615° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 287.5666° |
| argument of perigee: | 97.7004° |
| revolutions per day: | 15.30177562 |
| mean anomaly at epoch: | 262.4134° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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