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 19257U 88053B 23152.21584243 .00000305 00000-0 10963-3 0 9990
2 19257 74.0464 177.0506 0021578 250.3595 178.1147 14.37841102831304
| Epoch (UTC): | 01 June 2023 05:10:48 |
| Eccentricity: | 0.0021578 |
| inclination: | 74.0464° |
| perigee height: | 750 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 177.0506° |
| argument of perigee: | 250.3595° |
| revolutions per day: | 14.37841102 |
| mean anomaly at epoch: | 178.1147° |
| orbit number at epoch: | 83130 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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