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 47745U 26145.52499807 +.00000000 +00000-0 +66373-3 0 00000
2 47745 53.1547 196.4895 0007028 355.3819 4.7127 15.55495841 05
| Epoch (UTC): | 25 May 2026 12:35:59 |
| Eccentricity: | 0.0007028 |
| inclination: | 53.1547° |
| perigee height: | 396 km |
| apogee height: | 405 km |
| right ascension of ascending node: | 196.4895° |
| argument of perigee: | 355.3819° |
| revolutions per day: | 15.55495841 |
| mean anomaly at epoch: | 4.7127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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