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 47287U 26145.52527157 +.00000000 +00000-0 -94108-3 0 00009
2 47287 87.8959 355.1537 0001987 93.7902 266.3453 13.12441878 08
| Epoch (UTC): | 25 May 2026 12:36:23 |
| Eccentricity: | 0.0001987 |
| inclination: | 87.8959° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.1537° |
| argument of perigee: | 93.7902° |
| revolutions per day: | 13.12441878 |
| mean anomaly at epoch: | 266.3453° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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