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 47280U 26145.55929641 +.00000000 +00000-0 +87954-3 0 00009
2 47280 87.8963 355.1443 0001489 82.9865 277.1433 13.12442947 03
| Epoch (UTC): | 25 May 2026 13:25:23 |
| Eccentricity: | 0.0001489 |
| inclination: | 87.8963° |
| perigee height: | 1213 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.1443° |
| argument of perigee: | 82.9865° |
| revolutions per day: | 13.12442947 |
| mean anomaly at epoch: | 277.1433° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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