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 23152.82456698 .00020657 00000-0 61993-3 0 9992
2 25527 85.5239 181.1171 0005613 16.5296 343.6136 15.34315313348818
| Epoch (UTC): | 01 June 2023 19:47:22 |
| Eccentricity: | 0.0005613 |
| inclination: | 85.5239° |
| perigee height: | 459 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 181.1171° |
| argument of perigee: | 16.5296° |
| revolutions per day: | 15.34315313 |
| mean anomaly at epoch: | 343.6136° |
| orbit number at epoch: | 34881 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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