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 03669U 69009A 23264.87872497 .00000251 00000-0 16177-3 0 9990
2 03669 88.4142 254.0455 1711877 104.8810 274.7413 11.29723374246898
| Epoch (UTC): | 21 September 2023 21:05:21 |
| Eccentricity: | 0.1711877 |
| inclination: | 88.4142° |
| perigee height: | 575 km |
| apogee height: | 3448 km |
| right ascension of ascending node: | 254.0455° |
| argument of perigee: | 104.8810° |
| revolutions per day: | 11.29723374 |
| mean anomaly at epoch: | 274.7413° |
| orbit number at epoch: | 24689 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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