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 15495U 85009B 23152.50050352 .00000483 00000-0 54477-4 0 9995
2 15495 82.5224 309.3100 0019721 356.4127 3.6943 14.84403542 51403
| Epoch (UTC): | 01 June 2023 12:00:43 |
| Eccentricity: | 0.0019721 |
| inclination: | 82.5224° |
| perigee height: | 601 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 309.3100° |
| argument of perigee: | 356.4127° |
| revolutions per day: | 14.84403542 |
| mean anomaly at epoch: | 3.6943° |
| orbit number at epoch: | 5140 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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