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 47263U 26145.12219538 +.00000000 +00000-0 +83822-3 0 00000
2 47263 87.8958 355.2370 0001757 84.9218 275.2111 13.12440608 04
| Epoch (UTC): | 25 May 2026 02:55:57 |
| Eccentricity: | 0.0001757 |
| inclination: | 87.8958° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.2370° |
| argument of perigee: | 84.9218° |
| revolutions per day: | 13.12440608 |
| mean anomaly at epoch: | 275.2111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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