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 45387U 26145.28819816 +.00000000 +00000-0 +10836-2 0 00001
2 45387 53.0208 93.3241 0008981 76.9224 283.2789 15.59021124 04
| Epoch (UTC): | 25 May 2026 06:55:00 |
| Eccentricity: | 0.0008981 |
| inclination: | 53.0208° |
| perigee height: | 384 km |
| apogee height: | 397 km |
| right ascension of ascending node: | 93.3241° |
| argument of perigee: | 76.9224° |
| revolutions per day: | 15.59021124 |
| mean anomaly at epoch: | 283.2789° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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