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 47268U 26145.33990277 +.00000000 +00000-0 +95495-3 0 00003
2 47268 87.8962 355.2039 0001621 85.3659 274.7655 13.12440958 05
| Epoch (UTC): | 25 May 2026 08:09:27 |
| Eccentricity: | 0.0001621 |
| inclination: | 87.8962° |
| perigee height: | 1213 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.2039° |
| argument of perigee: | 85.3659° |
| revolutions per day: | 13.12440958 |
| mean anomaly at epoch: | 274.7655° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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