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 23029.70118098 .00017673 00000-0 31376-3 0 9997
2 25544 51.6431 294.4821 0004694 288.5696 176.2208 15.50280552380313
| Epoch (UTC): | 29 January 2023 16:49:42 |
| Eccentricity: | 0.0004694 |
| inclination: | 51.6431° |
| perigee height: | 413 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 294.4821° |
| argument of perigee: | 288.5696° |
| revolutions per day: | 15.50280552 |
| mean anomaly at epoch: | 176.2208° |
| orbit number at epoch: | 38031 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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