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 48400U 26145.54732889 +.00000000 +00000-0 +14344-3 0 00002
2 48400 53.1594 335.3947 0001434 91.4373 268.6793 15.31707713 04
| Epoch (UTC): | 25 May 2026 13:08:09 |
| Eccentricity: | 0.0001434 |
| inclination: | 53.1594° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 335.3947° |
| argument of perigee: | 91.4373° |
| revolutions per day: | 15.31707713 |
| mean anomaly at epoch: | 268.6793° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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