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 41465U 16026B 23092.22720888 .00033419 00000-0 51837-3 0 9995
2 41465 97.0104 325.0261 0008705 145.4704 2.9417 15.53886520388158
| Epoch (UTC): | 02 April 2023 05:27:10 |
| Eccentricity: | 0.0008705 |
| inclination: | 97.0104° |
| perigee height: | 399 km |
| apogee height: | 411 km |
| right ascension of ascending node: | 325.0261° |
| argument of perigee: | 145.4704° |
| revolutions per day: | 15.53886520 |
| mean anomaly at epoch: | 2.9417° |
| orbit number at epoch: | 38815 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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