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 23156.78730455 .00006480 00000-0 32454-3 0 9994
2 16262 82.4753 264.2648 0008974 337.9517 22.1329 15.17183093 47854
| Epoch (UTC): | 05 June 2023 18:53:43 |
| Eccentricity: | 0.0008974 |
| inclination: | 82.4753° |
| perigee height: | 508 km |
| apogee height: | 520 km |
| right ascension of ascending node: | 264.2648° |
| argument of perigee: | 337.9517° |
| revolutions per day: | 15.17183093 |
| mean anomaly at epoch: | 22.1329° |
| orbit number at epoch: | 4785 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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