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 25544U 98067A 23088.08098380 .00030532 00000-0 54595-3 0 9991
2 25544 51.6421 5.4335 0005829 143.4013 50.0954 15.49721800389360
| Epoch (UTC): | 29 March 2023 01:56:37 |
| Eccentricity: | 0.0005829 |
| inclination: | 51.6421° |
| perigee height: | 413 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 5.4335° |
| argument of perigee: | 143.4013° |
| revolutions per day: | 15.49721800 |
| mean anomaly at epoch: | 50.0954° |
| orbit number at epoch: | 38936 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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