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 23083.58950542 .00000508 00000-0 34624-3 0 9997
2 03669 88.4087 274.3194 1712090 110.4247 268.8480 11.29662661226422
| Epoch (UTC): | 24 March 2023 14:08:53 |
| Eccentricity: | 0.1712090 |
| inclination: | 88.4087° |
| perigee height: | 575 km |
| apogee height: | 3448 km |
| right ascension of ascending node: | 274.3194° |
| argument of perigee: | 110.4247° |
| revolutions per day: | 11.29662661 |
| mean anomaly at epoch: | 268.8480° |
| orbit number at epoch: | 22642 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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