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 47392U 26145.59686312 +.00000000 +00000-0 +74499-3 0 00002
2 47392 53.0455 357.7022 0002748 103.4541 256.6784 15.75787854 09
| Epoch (UTC): | 25 May 2026 14:19:28 |
| Eccentricity: | 0.0002748 |
| inclination: | 53.0455° |
| perigee height: | 341 km |
| apogee height: | 344 km |
| right ascension of ascending node: | 357.7022° |
| argument of perigee: | 103.4541° |
| revolutions per day: | 15.75787854 |
| mean anomaly at epoch: | 256.6784° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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