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 23088.26221505 .00024873 00000-0 44665-3 0 9996
2 25544 51.6425 4.5351 0005716 143.4859 341.7493 15.49718085389397
| Epoch (UTC): | 29 March 2023 06:17:35 |
| Eccentricity: | 0.0005716 |
| inclination: | 51.6425° |
| perigee height: | 413 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 4.5351° |
| argument of perigee: | 143.4859° |
| revolutions per day: | 15.49718085 |
| mean anomaly at epoch: | 341.7493° |
| orbit number at epoch: | 38939 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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