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 57848U 26145.10498319 +.00000000 +00000-0 +54345-4 0 00003
2 57848 53.1608 289.2129 0001360 90.7042 269.4114 15.30194331 09
| Epoch (UTC): | 25 May 2026 02:31:10 |
| Eccentricity: | 0.0001360 |
| inclination: | 53.1608° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 289.2129° |
| argument of perigee: | 90.7042° |
| revolutions per day: | 15.30194331 |
| mean anomaly at epoch: | 269.4114° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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