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 54252U 26145.66124626 +.00000000 +00000-0 +53679-3 0 00005
2 54252 97.6190 288.7947 0004639 87.4926 272.6861 15.59818562 07
| Epoch (UTC): | 25 May 2026 15:52:11 |
| Eccentricity: | 0.0004639 |
| inclination: | 97.6190° |
| perigee height: | 385 km |
| apogee height: | 391 km |
| right ascension of ascending node: | 288.7947° |
| argument of perigee: | 87.4926° |
| revolutions per day: | 15.59818562 |
| mean anomaly at epoch: | 272.6861° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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