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 data is extracted from the following two-line orbital elements,
1 25527U 98066A 23154.58547754 .00015350 00000-0 45980-3 0 9993
2 25527 85.5233 180.0479 0005284 10.1399 349.9956 15.34373809349082
| Epoch (UTC): | 03 June 2023 14:03:05 |
| Eccentricity: | 0.0005284 |
| inclination: | 85.5233° |
| perigee height: | 459 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 180.0479° |
| argument of perigee: | 10.1399° |
| revolutions per day: | 15.34373809 |
| mean anomaly at epoch: | 349.9956° |
| orbit number at epoch: | 34908 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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