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 16262U 85108A 23149.79605019 .00005457 00000-0 27366-3 0 9993
2 16262 82.4743 271.2079 0009537 2.0659 358.0612 15.17102653 46793
| Epoch (UTC): | 29 May 2023 19:06:18 |
| Eccentricity: | 0.0009537 |
| inclination: | 82.4743° |
| perigee height: | 508 km |
| apogee height: | 521 km |
| right ascension of ascending node: | 271.2079° |
| argument of perigee: | 2.0659° |
| revolutions per day: | 15.17102653 |
| mean anomaly at epoch: | 358.0612° |
| orbit number at epoch: | 4679 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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