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 23158.02582541 .00035987 00000-0 62302-3 0 9994
2 25544 51.6423 18.9165 0005198 59.7671 85.8503 15.50559272400218
| Epoch (UTC): | 07 June 2023 00:37:11 |
| Eccentricity: | 0.0005198 |
| inclination: | 51.6423° |
| perigee height: | 411 km |
| apogee height: | 418 km |
| right ascension of ascending node: | 18.9165° |
| argument of perigee: | 59.7671° |
| revolutions per day: | 15.50559272 |
| mean anomaly at epoch: | 85.8503° |
| orbit number at epoch: | 40021 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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