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 16613U 86019A 23156.58802743 .00000833 00000-0 14039-3 0 9999
2 16613 98.7503 4.3478 0141174 121.1777 240.3354 14.66190610648408
| Epoch (UTC): | 05 June 2023 14:06:45 |
| Eccentricity: | 0.0141174 |
| inclination: | 98.7503° |
| perigee height: | 574 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 4.3478° |
| argument of perigee: | 121.1777° |
| revolutions per day: | 14.66190610 |
| mean anomaly at epoch: | 240.3354° |
| orbit number at epoch: | 64840 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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